Possibly developed in the late-1980s, the highly classified two-stage-to-orbit "Blackstar" system could place a small payload in low Earth orbit or serve as a rapid-response reconnaissance platform. The two vehicles were seen several times throughout the 1990s, but may have been shelved in recent years, according to officials familiar with the program (see p. 48). Graphic by James Petty and Travis Thatcher.
========
Two-Stage-to-Orbit 'Blackstar' System Shelved at Groom Lake?
Aviation Week & Space Technology, 03/06/2006, page 48
William B. Scott, Colorado Springs
For 16 years, Aviation Week & Space Technology has investigated myriad sightings of a two-stage-to-orbit system that could place a small military spaceplane in orbit. Considerable evidence supports the existence of such a highly classified system, and top Pentagon officials have hinted that it's "out there," but iron-clad confirmation that meets AW&ST standards has remained elusive. Now facing the possibility that this innovative "Blackstar" system may have been shelved, we elected to share what we've learned about it with our readers, rather than let an intriguing technological breakthrough vanish into "black world" history, known to only a few insiders.
U.S. intelligence agencies may have quietly mothballed a highly classified two-stage-to-orbit spaceplane system designed in the 1980s for reconnaissance, satellite-insertion and, possibly, weapons delivery. It could be a victim of shrinking federal budgets strained by war costs, or it may not have met performance or operational goals.
This two-vehicle "Blackstar" carrier/orbiter system may have been declared operational during the 1990s.
A large "mothership," closely resembling the U.S. Air Force's historic XB-70 supersonic bomber, carries the orbital component conformally under its fuselage, accelerating to supersonic speeds at high altitude before dropping the spaceplane. The orbiter's engines fire and boost the vehicle into space. If mission requirements dictate, the spaceplane can either reach low Earth orbit or remain suborbital.
The manned orbiter's primary military advantage would be surprise overflight. There would be no forewarning of its presence, prior to the first orbit, allowing ground targets to be imaged before they could be hidden. In contrast, satellite orbits are predictable enough that activities having intelligence value can be scheduled to avoid overflights.
Exactly what missions the Blackstar system may have been designed for and built to accomplish are as yet unconfirmed, but U.S. Air Force Space Command (AFSPC) officers and contractors have been toying with similar spaceplane-operational concepts for years. Besides reconnaissance, they call for inserting small satellites into orbit, and either retrieving or servicing other spacecraft. Conceivably, such a vehicle could serve as an anti-satellite or space-to-ground weapons-delivery platform, as well.
A two-stage-to-orbit system developed during the late 1980s consists of a large XB-70-like aircraft and small spaceplane carried semi-conformally. Credit: JAMES PETTY AND TRAVIS THATCHER
Once a Blackstar orbiter reenters the atmosphere, it can land horizontally at almost any location having a sufficiently long runway. So far, observed spaceplane landings have been reported at Hurlburt AFB, Fla.; Kadena AB, Okinawa; and Holloman AFB, N.M.
The spaceplane is capable of carrying an advanced imaging suite that features 1-meter-aperture adaptive optics with an integral sodium-ion-sensing laser. By compensating in real-time for atmospheric turbulence-caused aberrations sensed by the laser, the system is capable of acquiring very detailed images of ground targets or in-space objects, according to industry officials familiar with the package.
THE SPACEPLANE'S SMALL CARGO or "Q-bay" also could be configured to deliver specialized microsatellites to low Earth orbit or, perhaps, be
fitted with no-warhead hypervelocity weapons--what military visionaries have called "rods from god." Launched from the fringes of space, these high-Mach weapons could destroy deeply buried bunkers and weapons facilities.
While frequently the subject of advanced studies, such as the Air Force's "Spacecast 2020," actual development and employment of a transatmospheric spaceplane have not been confirmed officially (AW&ST Sept. 5, 1994, p. 101). However, many sightings of both an XB-70-like carrier and a spaceplane have been reported, primarily in the western U.S. Only once have they been seen together, though.
On Oct. 4, 1998, the carrier aircraft was spotted flying over Salt Lake City at about 2:35 p.m. local time. James Petty, the president of JP Rocket Engine Co., saw a small, highly swept-winged vehicle nestled under the belly of the XB-70-like aircraft. The vehicle appeared to be climbing slowly on a west-southwest heading. The sky was clear enough to see both vehicles' leading edges, which Petty described as a dark gray or black color.
For whatever reason, top military space commanders apparently have never been "briefed-in"--never told of the Blackstar system's existence--even though these are the "warfighters" who might need to employ a spaceplane in combat. Consequently, the most likely user is an intelligence agency. The National Reconnaissance Office may have played a role in the program, but former senior NRO officials have denied any knowledge of it.
One Pentagon official suggests that the Blackstar system was "owned" and operated by a team of aerospace contractors, ensuring government leaders' plausible deniability. When asked about the system, they could honestly say, "we don't have anything like that."
The "XOV," or experimental orbital vehicle, has a short, flat-topped vertical fin that may double as a mounting pylon. A "Q-bay" aft of the cockpit could carry small payloads.
Aerospace industry contractors suggest that a top secret Blackstar system could explain why Pentagon leaders readily offered the Air Force's nascent unclassified spaceplane project, the briefly resurrected SR-71 program and the Army's anti-satellite program for elimination from budgets in the late 1990s. At the time, an industry official said, "if we're flying a spaceplane, it makes sense to kill these cover programs and stop wasting money on things we can already do."
U.S. and European aerospace companies have pushed two-stage-to-orbit (TSTO) spaceplane concepts for decades. Most large U.S. airframe manufacturers designed spaceplane-type vehicles during the 1950s and '60s, and XB-70 program documents include a concept for carrying and launching a low-Earth orbiter. Two former test pilots and executives for North American Aviation (later, Rockwell) said the company had a technically viable plan for such a system in the 1950s (AW&ST Aug. 24, 1992, p. 25).
Boeing is believed to be one of several major aerospace companies involved in the Blackstar program. On Oct. 14, 1986, Boeing filed a U.S. patent application for an advanced two-stage space transportation system. Patent No. 4,802,639, awarded on Feb. 7, 1989, details how a small orbiter could be air-dropped from the belly of a large delta-winged carrier at Mach 3.3 and 103,800-ft. altitude. The spaceplane would be boosted into orbit by its own propulsion system, perform an intended mission, then glide back to a horizontal landing. Although drawings of aircraft planforms in the Boeing patent differ from those of the Blackstar vehicles spotted at several USAF bases, the concepts are strikingly similar.
One logical explanation given for why a Blackstar system is developed says that, after the shuttle Challenger disaster in January 1986, and a subsequent string of expendable-booster failures, Pentagon leaders were stunned to learn they no longer had "assured access to space." Suddenly, the U.S. needed a means to orbit satellites necessary to keep tabs on its Cold War adversaries.
A team of contractors apparently stepped forward, offering to build a quick-reaction TSTO system in record time. The system could ensure on-demand overflight reconnaissance/surveillance from low Earth orbit, and would require minimal development time.
Tons of material--including long-lead structural items--for a third XB-70 Valkyrie had been stored in California warehouses years before, and a wealth of data from the X-20 DynaSoar military spaceplane program was readily available for application to a modern orbiter (see following articles).
DYNASOAR WAS TERMINATED shortly after President John F. Kennedy was assassinated in 1963, after $430 million had been spent on the spaceplane's development. Political opposition and the fatal crash of XB-70 No. 2 on June 8, 1966, contributed to the bomber program's being canceled before Air Vehicle No. 3 could be built. However, at one time, there had been plans to mate the two vehicles.
In XB-70 Valkyrie: The Ride to Valhalla, Jeannette Remak and Joe Ventolo, Jr., wrote: "One version of the B-70 could have been used as a recoverable booster system to launch things into low-Earth orbit. . . . The DynaSoar program, the first effort by the [U.S.] to use a manned boost-glider to fly in near-orbital space and return, was considered in this context in November 1959. The B-70 was to carry the 10,000-lb. DynaSoar glider and a 40,000-lb. liquid rocket booster to 70,000 ft. and release them while traveling at Mach 3. With this lofty start, the booster could then push the glider into its final 300-mi. orbit."
The two-stage U.S. spaceplane concept apparently has undergone several iterations since then, but the basic idea remained--launch a manned boost-glide vehicle from an XB-70-like platform (AW&ST Dec. 24, 1990, p. 48; Sept. 24, 1990, p. 28). An aerospace industry source said the Air Force once used the "Blackstar" moniker, but others suggested the intelligence community referred to this TSTO combination as the "SR-3/XOV" system. The SR-3 is the large, XB-70-like carrier aircraft, while the small orbital vehicles drop-launched at high speed are called XOV-1, XOV-2 and so forth. At one time, the XOV designator meant "experimental orbital vehicle."
Based on information gleaned from multiple industry sources, the SR-3 features:
*A roughly 200-ft.-long, clipped-delta-winged planform resembling that of the North American Aviation XB-70 trisonic bomber. The forward fuselage is believed to be more oval-shaped than was depicted in a 1992 artist's rendering (AW&ST Aug. 24, 1992, p. 23).
*Canards that extend from the forward fuselage. These lifting surfaces may sweep both fore and aft to compensate for large center-of-gravity changes after dropping the spaceplane, based on multiple sighting reports.
*Large, outward-canted vertical tail surfaces at the clipped-delta's wingtips.
*At least four engine exhaust ports, grouped as two well-separated banks on either side of the aircraft centerline.
*Very loud engines. One other classified military aircraft may have used the same type of powerplant.
*Operation at supersonic speeds and altitudes up to 90,000 ft.
During the system's development cycle, two types of spaceplane orbiters may have been flown. Both were a blended wing/fuselage lifting-body design, but differed in size. The smaller version was about 60-65 ft. long and may have been unmanned or carried a crew of two, some say. Industry engineers said this technology demonstrator was "a very successful program."
The larger orbiter is reportedly 97.5 ft. long, has a highly swept, blended wing/body planform and a short vertical fin. This bulky fin apparently doubles as a buried pylon for conformal carriage of the spaceplane beneath the large SR-3. The "Q-bay" for transporting an optics-system pallet or other payloads may be located aft of the cockpit, with payload doors on top of the fuselage.
Outboard sections of the spaceplane's wing/body cant slightly downward, possibly for shock-wave control and compression lift at high speeds while in the atmosphere, whether on ascent or reentry. The only visible control surfaces are flap- or drag-type panels on the wing's trailing edge, one section on each side of the stubby vertical fin. A relatively large, spade-shaped section forward of the cockpit--which gives the orbiter a "shark-nose" appearance--may provide some pitch stability, as well.
The orbiter's belly appears to be contoured with channels, riblets or "strakelets" that direct airflow to engine inlets and help dissipate aerodynamic heating. These shallow channels may direct air to a complex system of internal, advanced composite-material ducts, according to an engineer who says he helped build one version of the orbiter in the early 1990s. Air is directed to what is believed to be aerospike engines similar to those once planned for use on the NASA/Lockheed Martin X-33.
A former Lockheed Skunk Works official once expressed confidence in the X-33 prototype orbiter's powerplants, noting that "they have history." Whether this implies the aerospikes had flown before, perhaps on an XOV, or simply referred to ground test-firings is unknown. The X-33 was a prototype of what was to be the single-stage-to-orbit Venture Star (AW&ST Nov. 10, 1997, p. 50).
Technicians who worked at a McDonnell Douglas plant in St. Louis in the late 1980s and early 1990s said much of the XOV's structure was made of advanced composite materials. Some wing skin panels measured 40 ft. long and 16 ft. wide, yet were only 3/8 in. to 1/2 in. thick.
"Two people could pick them up; they were very light," one said. These panels were stacked in a sandwich structure to obtain the required thickness, then machined to shape. Although much of the structure was honeycomb, it was "incredibly strong, and would handle very high temperatures," he noted. Inside skin surfaces "were ungodly complicated," though.
WORK ON THE ORBITER moved at a relatively slow pace until a "fuel breakthrough" was made, workers were told. Then, from 1990 through 1991, "we lived out there. It was a madhouse," a technician said. The new fuel was believed to be a boron-based gel having the consistency of toothpaste and high-energy characteristics, but occupying less volume than other fuels.
Regardless of where they land, spaceplane orbiters usually are retrieved by one or more "fat" C-5 Galaxy transports. Three of the oversized aircraft were modified with 8-ft.-wide "chipmunk cheek" extensions on each side of the cargo compartment aft of the nose hinge point; an extra six-wheel set of landing gear that partially retracts up against the aft fuselage, forward of the ramp; a shortened upper deck, and two internal harness/cradle supports. These alterations originally were made to enable carriage of dome-topped containers measuring 61.2 ft. long, 17.2 ft. wide (maximum) and 16.7 ft. tall at the highest point. The containers normally protected satellites during transit to launch sites.
In 1994, NASA sources confirmed that two of the C-5s (Tail Nos. 00503 and 00504) were listed on NASA's inventory--although the aircraft did not "officially" exist, according to the agency's public records. Both transports apparently were deployed only upon orders from the administrator's office. The third oversized C-5 once had a red "CL" on its tail, and supposedly was used by the Central Intelligence Agency. All three C-5s may have been retired in recent years, according to a NASA contractor.
CRITICS ARGUE that there was never enough money hidden in intelligence and military budgets to fund a small fleet of spaceplanes and carrier aircraft. However, those who worked on the system's development at several contractor sites say they charged time-and-materials costs to a number of well-funded programs. Lockheed was the lead contractor for Blackstar orbiters being fabricated at McDonnell Douglas in the early 1990s, and workers there typically logged their time against a specific Lockheed charge number associated with that project. But their time might also have been charged to the National Aero-Space Plane (NASP) and the Navy's A-12 fighter accounts, they say. Both multibillion-dollar programs were canceled with little but technology development gains to show for massive expenditures.
"At first, [supervisors] said we were working on NASP, but this thing never looked like anything the public was shown," a McDonnell Douglas technician who worked in the company's "black hole" facility said. "Later, we were just told, 'Clock it to NASP and don't ask questions.' We never did anything that was really NASP--and money was never a problem."
Whether the Blackstar system was ever declared operational or not is unknown, but several orbiters may have flown over the years. A former program manager at a major aerospace company once declared, "There's no question; Lockheed is flying a two-stage space vehicle."
Interestingly, after both Lockheed and Boeing pulled out of the NASP competition (or were "eliminated") in the 1980s, they may have collaborated to develop the two-stage-to-orbit Blackstar system under a highly classified "fast-track" program. However, many other contractors' "deep-black" teams probably also were involved in order to bring the nation's best expertise to bear on what must have been daunting technical challenges.
================
Secret Spaceplane May Have Suffered Damage During Air-Launch
Aviation Week & Space Technology, 03/06/2006, page 50
William B. Scott, Colorado Springs
Air-dropped spaceplane described as a transatmospheric 'boost-glide' vehicle
Sighting reports from fighter pilots, civilian contractors and an Air Force security police officer provided enough information about a super-secret "black" spaceplane to develop a technical profile of the vehicle. Both manned and unmanned versions may have been test-flown and operated during the last 16 years.
The two-vehicle Blackstar system's spaceplane has been referred to as "Black Magic," "Speedy" and "XOV" (experimental orbital vehicle) over the years, but none of these monikers have been confirmed by high-level U.S. government representatives. Intelligence officials called it the XOV, and that designation seems to be the most accepted in "black world" circles.
In general, transatmospheric vehicles have been classed as "boost-glide" craft for decades. Such vehicles would be boosted into space by internal powerplants, but returned to Earth unpowered.
A manned XOV was spotted at Holloman AFB, N.M., in 1994 by an F-15 crew chief as he prepared a fighter for an early morning flight. He alerted the pilot, who immediately climbed into the Eagle's cockpit and, using a small pair of binoculars, watched activities associated with the XOV/spaceplane for some time. He made a detailed sketch of the vehicle, and described it as follows:
*A 90-100-ft.-long, highly swept-winged, blended and contoured lifting body. The outer wing surfaces drooped or curved downward slightly, suggesting the spaceplane used compressive-lift techniques, while in the atmosphere.
*The vehicle's belly was "grooved" with longitudinal channels, possibly 1-2 ft. deep.
*It had a longitudinally lengthy, but unusually short vertical fin that could double as a carriage/launch pylon. The F-15 pilot said the vertical tail structure was partially covered with a tarp, but the aft portion of the tail fin/pylon appeared to be missing or damaged.
*A retractable nose gear sported several small wheels. A large, ski-like skid was mounted under the fuselage centerline, and two outrigger "pogo"-type wheeled gear supported each wing's outboard section.
*The only control surfaces observed were flap- or elevon-type panels at the wing's trailing edge on each side of the stubby vertical fin. Both panels were raised at the time.
The XOV spaceplane has an odd spade-shaped forward-body planform, according to observers. The underbelly exhibits a series of grooves, riblets or "strakelets" that may improve heat dissipation during reentry or channel air to internal engines. Credit: JAMES PETTY AND TRAVIS THATCHER
*Four rectangular engine exhaust grates on the blunt rear surface of the vehicle. Two of these sections were seen on each side of the vertical fin, and described as "screened or radiator-like." This suggests that linear aerospike engines might power the spaceplane.
*Outboard of each rectangular engine-exhaust bank, near the highly swept delta planform's wingtips, was a single round port--possibly the nozzle of a reusable solid rocket booster. Observers at other locations have reported seeing long cylindrical pods lying on the ground near the spaceplane. Each pod was painted white with red stripes on each end. They speculated that these pods were boosters that could be inserted like shotgun shells into the outboard receptacles.
The Holloman F-15 pilot's sighting came only days after an unusual incident near Okinawa that may or may not have been related. In early 1994, fighter pilots flying in that area were briefly diverted to allow "an aircraft in distress" to land at Kadena AB, according to air traffic control transmissions.
An F-15 pilot obtained a radar lock on the vehicle, providing a data readout that supposedly indicated the "aircraft in distress" was at a high-supersonic speed and descending steeply, as it passed through about 45,000 ft. The unidentified aircraft landed at Kadena, and the base was immediately "locked down," a pilot said. Kadena employees, flight crews and contractors were prevented from leaving the base for a period. A civilian contractor who saw the spaceplane land was "debriefed" and hustled off-base within hours.
Possibly the same day, a modified "fat" C-5 left Holloman AFB on a "northern Pacific route," then returned within a week. That's when the Holloman-based F-15 pilot and his crew chief saw the boost-glide vehicle (during daylight hours). The pilot postulated that the spaceplane's vertical fin/pylon had been damaged, perhaps during launch over the Pacific, forcing the vehicle to make an emergency landing at Kadena.
Attempts to confirm both the Kadena-area and Holloman incidents have been unsuccessful.
"Big. White or beige color. Very loud. I've never seen an airplane like it."
Those are typical descriptions from people who reported seeing an unusual aircraft, yet who characterize themselves as "not that familiar with airplanes."
But others who saw the same vehicle, and did know their aircraft, typically said something like: "Well . . . you're going to think I'm crazy . . . but it looked like the old XB-70--the Valkyrie. But there were only two of those built. One crashed, and the other's in the [National Museum of the] Air Force [in Dayton, Ohio]. So it couldn't have been an XB-70, right?"
About a dozen such reports have found their way to Aviation Week & Space Technology since 1990, often accompanied by rough sketches of the large aircraft. The most recent came last year from a retired test pilot living in the southern U.S. He saw the aircraft on a Sunday afternoon, and described the "loud rumbling" noise usually mentioned in sighting reports.
Two XB-70-like spaceplane carriers may have been built. One might have crashed, and a second is stored at the USAF's secret Groom Lake test site in Nevada, says an industry source. We've long suspected these aircraft were launch platforms, but that wasn't confirmed until James Petty, a rocket company president based in Salt Lake City, saw the white "mothership" carrying a small vehicle under its aft fuselage on Oct. 4, 1998 (see p. 48).
Ostensibly designated the SR-3, the XB-70-like aircraft is believed to be a supersonic, high-altitude launch platform for the highly classified "XOV" spaceplane (see p. 52).
It differs from the XB-70 in several ways, though.
DETAILED FEATURES of the aircraft were provided by Nancy Weitzman, who was then a Ph.D. candidate living in Doylestown, Pa., and saw the SR-3 overfly her home in 1993. The aircraft was at an altitude of roughly 2,500 ft. and only a half-mile from Weitzman. She said it was close enough to see one pilot's helmet. Initially, the vehicle was maneuvering at slow speed and banking, offering excellent views of its top, bottom and tail sections. It then accelerated and climbed at a steep angle with all engines in afterburner, creating an incredibly loud noise.
While not "an airplane person," in her words, Weitzman is a longtime bird-watcher, and was a medical student then, making her an excellent, detail-oriented observer. Her engineer husband enhanced her sighting report by providing the correct aeronautical terminology for certain features. Based on her detailed description, plus tidbits provided by other observers, the following profile of the SR-3 "carrier" was constructed by Aviation Week:
*The SR-3 is a 180-200-ft.-long, light-colored, clipped-delta-winged aircraft that closely resembles the 1960s-vintage North American XB-70 bomber.
*Movable canards are mounted at mid-fuselage height aft of the cockpit. Weitzman reported the canards swept forward; others said they were swept aft, opening the possibility that canards may be positioned manually or automatically, depending on flight conditions.
*A dorsal ridge extends along the SR-3's spine from the cockpit to near the delta's trailing edge, enhanced by a dark line running at least two-thirds of the aircraft's length (AW&ST Aug. 24, 1992, pp. 23 and 25).
*Upward-swept "sails" or vertical tail surfaces are canted outward and mounted at the delta planform's wingtips.
*At least four engine exhaust ports are grouped as two well-separated banks, with ports on each side of the aircraft's centerline.
The XB-70-like "mothership" could deploy an XOV spaceplane at supersonic speeds and altitudes up to 90,000 ft. The spaceplane may be embedded conformally under the carrier aircraft's aft fuselage. Credit: JAMES PETTY AND TRAVIS THATCHER
*Its belly is not aerodynamically smooth. Weitzman said the aircraft had several blended, curved areas and a large "hump" on the centerline, flanked by two smaller humps aft of two engine inlets. She likened the blended-body contours to the B-2 bomber's upper fuselage. These may ensure a small spaceplane can be carried conformally.
*A distinctive deep, rumbling, very loud engine noise.
Several SR-3 vehicles could have been built fairly quickly from material that had been delivered for XB-70 Air Vehicle No. 3 (AV-3). Work on AV-3 ceased when its contract was canceled on Feb. 15, 1964. However, more than 24,000 sq. ft. of honeycomb-core material, 157,000 lb. of sheet metal and 26,000 ft. of metal extrusions had already been delivered for AV-3, according to public records.
Tony Landis, a coauthor of North American XB-70A Valkyrie (published in 2002 as Vol. 34 of the Warbird Tech series), said his research "never found any reference to the disposal of six or seven warehouses-full of spare parts for the XB-70."
A former vice president of engineering, who oversaw XB-70 development at North American Aviation (NAA) for a brief period, says several SR-3 aircraft could have been built relatively quickly. However, they probably would have been fabricated from aluminum, not the XB-70's complex honeycomb material, because the SR-3 would not have to survive the high-heating stresses of Mach 3 speeds. Launching a spaceplane at Mach 1-2 would have been sufficient, greatly simplifying SR-3 construction, he notes.
Furthermore,
15 General Electric YJ-93-3 engines built specifically for the XB-70/B-70 program seem to have disappeared. "Apparently, there are no records available . . . showing any actions that may have been taken to scrap the engines. They simply don't appear on any inventory list. At last report, General Electric Aircraft Engines was still researching this matter," wrote Jeannette Remak and Joe Ventolo, Jr., in their comprehensive 1998 book, XB-70 Valkyrie: The Ride to Valhalla.
Overall, a two-stage-to-orbit system wouldn't have been technologically difficult to develop, according to aerospace veterans. A former NAA test pilot says, "We could have done it in the 1950s. The only reason we didn't was the expendable [rocket] guys got out ahead of us--and the rest is history."
10kBq Jaro included: ... Exactly what missions the Blackstar system may have been designed for and built to accomplish are as yet unconfirmed, but U.S. Air Force Space Command (AFSPC) officers and contractors have been toying with similar spaceplane-operational concepts for years. Besides reconnaissance, they call for inserting small satellites into orbit, and either retrieving or servicing other spacecraft. Conceivably, such a vehicle could serve as an anti-satellite or space-to-ground weapons-delivery platform, as well.
... The spaceplane is capable of carrying an advanced imaging suite that features 1-meter-aperture adaptive optics with an integral sodium-ion-sensing laser. By compensating in real-time for atmospheric turbulence-caused aberrations sensed by the laser, the system is capable of acquiring very detailed images of ground targets or in-space objects, according to industry officials familiar with the package.
An air-breathing first stage?
The painting shows a B-70 look-alike with a very large object under its belly, which is already protruberant with large air intakes. Landing legs would have to be, like, 15 metres long, minimum. As artistically impressioned, there is no sign of landing gear at all.
The real thing would have been handy for checking out Columbia's launch damage, maybe repairing it, maybe providing the astronauts an alternate ride home. Secrecy might have required that we never hear of Columbia's trouble-that-wasn't. Yeah, that's the ticket. They'd never compromise secrecy just for a little glory.
Graham, I had the same concern when I first saw the illustrations.
However, the article says that "A large "mothership," closely resembling the U.S. Air Force's historic XB-70 supersonic bomber, carries the orbital component conformally under its fuselage....."
Although I don't work in the aerospace industry, I heard that "conformal component" means that its carried flush with the fuselage, as for example the conformal fuel tanks on the F-18 (the plane may also carry external fuel tanks, which are much more easily discerned).
Now although the Blackstar illustration shows the XOV apparently suspended below the mothership like a big bomb, it seems to me that any such vehicle carried conformally from runway take-off to Mach-3 at high altitude, would first need to be lowered mechanically, before release.
So the illustration may simply be showing the deployed stage just prior to release.
In the conformal position, the XOV would be virtually invisible.
Anyway, that's one possibility, if you haven't made up your mind yet whether this is pure fiction or not....
Aviation Week & Space Technology, 03/27/2006, page 9
James R. French, Las Cruces, N.M.
Fascinating as it may sound, the BlackStar article does not meet the test of credibility (AW&ST Mar. 6, p. 48).
Based upon some quick analysis by my colleague Chuck Deiterich, a vehicle launching due east (to take advantage of the Earth's rotation) at Mach 3.3 would still require a delta velocity of about 21,700 ft./sec. to reach orbit. This doesn't account for drag losses, which even at that altitude probably would be 200 ft./sec.
The best performance I have seen for a boron fuel, even with highly toxic liquid fluorine as an oxidizer, is a specific impulse of 409-412 sec. using a 95% efficiency. This will require a start-of-burn/end-of-burn mass ratio of around 5:2-- not difficult for a disposable stage but challenging for a manned vehicle with crew and payload, which must bear the weight of an entry thermal protection system, landing gear, etc. Using more probable oxidizers, the ratio quickly becomes impractical.
The description of the vehicle goes on at length about apparent inlets on the belly. This is entirely at odds with the discussion of the linear aerospike rocket engine. The only air-breather that might be useful in this flight regime is the scramjet, which, while it does use an external expansion nozzle, does not use a linear aerospike of the type depicted. (Incidentally, the illustrations show a lack of comprehension about how a linear aerospike works.) Also, it seems unlikely that a scramjet would work with a slurry fuel as described, since the solid particles will be slow to mix and burn while rapidity is crucial to a scramjet.
Finally, the B-70 launch of a "40,000-lb. stage" carrying a "10,000-lb. Dynasoar" surfaces again. Using the delta-V values quoted above, this combination is incapable of reaching orbit. Even if we use the specific impulse of the Space Shuttle Main Engine and ascribe an improbable 0.9 propellant mass fraction to the stage, it falls about 3,000 ft./sec. short.
One wonders how these ideas persist without anyone ever really checking the numbers. I could go on at great length about other improbabilities, but this is enough. I really hope I'm wrong and that some super-duper vehicle does reside out there in the black world. I don't think I'll hold my breath, however.
Hmmm. Still, it makes me wonder if the vehiclw was possibly a flying testbed to test smaller hypersonic vehicles: possibly a hypersonic high altitude reconaissance vehicle. One was rumored to exist that used external supersonic combustion to generate thrust. It was rumored to have been called "Pumpkin Seed" because of its similarity in shape--kind of a double arrowhead, with flat angular plates. The shape was stealthy, yet it created expansion shocks at the widest point that could trap hot gasses. Supposedly propellant like methane was injected just ahead of this region where hot air supported supersonic combustion. The hot gasses exapnded to fill the region of lower pressure created by the expansion shocks. The result was that the gasses expand across the back of the vehicle and generate thrust. The vehicle in effect is the engine--and the entire outer surface was a SCRAMJET engine.
I don't know if this is true, but it seems plausible. Maybe this "Valkerie-like" vehicle is a dropship for small hypersonic experimental UAVs and UCAVs.
Aviation Week & Space Technology, 04/10/2006, page 7
A. Leroy Clarke, Santa Fe, N.M.
As a former wind tunnel engineer, the possibility of an "XB-70 like spaceplane carrier" (AW&ST Mar. 6, p. 48) was of interest.
The artist's sketch of the mated version certainly would illustrate a challenge for the landing gear group. The spaceplane likely would have to be much smaller or flatter than was pictured to have any hope of being strut-mounted to a large mothership needing to take off from a runway with conventional landing gear.
The spaceplane could have been partially submerged into the fuselage in place of the bomb bays, similar to the X planes in B-29s. B-70 bays were large enough to enclose the 1950s generation of nuclear stores, which were big and heavy. Better yet, the spaceplane could have been piggybacked on the aft fuselage, ahead of the vertical tails. Moving the XB-70's vertical tails outboard, as shown, would ease a launch from topside. This idea was studied in the late '50s. I conducted wind tunnel tests with the B-70 for a spaceplane launch at altitude.
One wonders at all of the supposed black (classified non-disclosed) areospace programs the U.S. might have. So far I've counted four. Each requiring its own unique airframe and in the case the Dark Star claim two of them! Let's first there was the Aurora then the TR-3A, the Jackknife (the supersonic figher with variable reverse swept back wings...F-14 meets X-29) and now the Dark Star! How do they hide all of the money plus the $50 billion for the Intel community?
This Dark Star would be uniquely expensive with a B-70 class launch platform and a spaceplane. I wonder if there isn't some sort of a on going government disinformation campaign that periodically puts this stuff in the press so as to confuse foreign intelligence services into wasting their efforts and to prepare against non-existent U.S. capabilities.
The following aircraft deployments began in the mid-1990's:
SR-3 FACTS:
1. SR-3 airframe is similar to the XB-70, EXCEPT canards and engine nacelle. Delta wing appears identical to XB-70 when at horizontal position.
2. On December 18, 1999 an SR-3 aircraft powered by Pulse Detonation Engine (PDE) propulsion made a cross country flight to southern California. Dryden test range was estimated destination.
3. PDE propulsion enables cruise speed between MACH 4-5. Takinging off from the east Coast after dark, the aircraft arrives at the west Coast at sunset.
4. Deployment: California
TR-3 FACTS:
1. Airframe is "flying wing" - delta wing, isosceles triangle configuration. with a smooth, slightly curved undercarriage and angled, or gabled-top.
2. Runs quiet, runs slow. Usually five aircraft fly practice missions together, but not in formation. Equipped with typical complement of regulation military aviation lights, including strobes and bright traffic approach beams.
3. TR-3 possesses four (4) vertical thrust vector ports for near-hover speeds of 35 knots.
4. Utilizes adaptive camouflage, projecting stars from background to smooth undercarriage during night flights.
5. Deployment: Nevada, New Mexico and Arizona military training facilities.
AC-X FACTS:
1. The AC-X uses a slightly modified C-130 airframe, with special nodules housing aiming lenses for the battle laser, microwave emitter, and a bright-white rotating warning beam which is activated prior to firing at the test range.
2. This Laser weapon platform has been firing bright-blue air-to-ground high energy laser beams at targets for over 10 years. Sound: Jacob's Ladder buzz.
3. Raytheon has been working on adding a high energy Mircowave weapon.
This Dark Star would be uniquely expensive with a B-70 class launch platform and a spaceplane. I wonder if there isn't some sort of a on going government disinformation campaign that periodically puts this stuff in the press so as to confuse foreign intelligence services into wasting their efforts and to prepare against non-existent U.S. capabilities.
Yea...I tend to agree with this. DOD has systems to deal with LEO threats to their milSATS without spending 'crazy' money on programs that are beyond realistic expectations they would perform without the system(s) ending up in enemy hands due to poor performance. What DOD should be doing in providing the best Intel on enemy location, capability to weaponize and deliver. I'm sure they already have the capability to deal effectively if they need to disable a real threat via typical methods without the space techie shock-and-awe.
Then, perhaps you have not yet seen one of these aircraft exercising its unique capabilities:
I watched one (1) flyover of the SR-3, or modified B-70, cruising at Mach 4 to 5, displaying the characteristic PDE wave contrail and heard the series of "booms" coming from the opposite horizon from whence it came. However, no space plane was attached to the undercarriage. The aircraft was viewed north of Prescott, Arizona, in Inscription Canyon with my nephew, who subsequently joined the Air Force.
I have viewed several Black Manta flights with one of the delta flying wings coming in low, overhead at close range. This was at night.
My neighbor was an eyewitness to (2) two consecutive air-to-ground firings of the AC-X (C-130) Laser gunship. According to his report, the laser was able to recharge and fire again fairly quickly (within minutes) - not bad for the 1990's!
You woudln't happen to have any video or pictures...?
The XB-70 was big, big plane. It was uniquely capable at Mach 3+ speeds and near 100,000 feet. It also had a tremendous payload for such a fast aircraft. However, the ground clearence beneath the 'air box' aft of the engine intakes leaves me to think that only fairly small vehicles could be placed here--conformally so that they are partially recessed. The XB-70 had some serious limitations and shortcomings for continued use as an operational craft...
One was the need for a rather large amount of freon (about 4 tons I think) that was used to actively cool the nose, electronics, and pilots cabin--otherwise the crew would cook like shrimp on a hot griddle! Much of the heat was dumped into the fuel, but an appreciable fraction of the heat was dumped with the warm freon boiloff--that freon had to be replenished each flight...
Some very nice infor and lots of good pictures of the NASA XB-70 at Dryden Air Force Base:
The XB-70 also used 6 General Electric YJ-93-3 turbojets with afterburners--I don't think the airframe could take the vibrations of the pulse detonation engines...and then there is the problem of cooling. I can imagine this airframe topping Mach 4--ultimate speed at 100,000 feet. But it can't do Mach 5 or 6--too much heating. The Titanium honeycomb substructure would require active cooling over the entire forward part of the body of the plane. This will consume far too much coolant to be practical. Only some kind of reusable refractory surface insulation--like the refractory metal tiles for proposed as a replace for Shuttle reusable TPS. It is unknown to me how heavy these metal tiles are--but they are heavier than silica-borosilicate glass tiles currently used on the Shuttle.
This is why I don't think the XB-70 can do mach 5 or six.
The vibration issues you describe are a real concern. The real success of PDE technology will be proven in interplanetary missions to Saturn's moons, etc on the next generation space craft. The ability to keep increasing speed and concerve fuel happens with the very low drag/friction environment of space. This may be why very few PDE flights are made today. I am blessed to have seen one. The donuts on a rope contrail, and series of sonic boom-like explosions are unmistakebly from a PDE.
Your points about heat build up and airframe material limitations would explain why the military / NSA are actively funding the new Falcon hypersonic aircraft for maintaining a cruise speed of approximately Mach 7. Raytheon was recently awarded a contract to work on the Falcon's hypersonic radar dome. We need to keep in mind that the SR-3 has been in service PRIOR to the SR-71 being mothballed. However, the SR-71 made a brief comeback suddenly about a dozen years ago. I suspected a crash of an SR-3 (although I did not know the SR-3 designation for the spy plane back then). A crash in New Mexico with "green flames" ocurred right before the de-mothballing of two SR-71s later the same month. SR-71 type fuel burns green.
I only have my sketchbook and / or artist renditions of these aircraft and the Falcon.
One interesting little fact: the afterburner of the "Port" (left) engine of an SR-71 burns Red while the Starboard (right) engine burns Green--the colorants (probably an organic salt of Strontium in the case of Red, and an organic salt of Copper in the case of the green flame) were actually injected into the fuel stream just prior to injection into the afterburners...
Pulse detonation engine technology is interesting--and may prove quite useful in increasing the fuel economy of 'conventional' subsonic aircraft, but I see no way for them to be used in a deep space craft--the resultant Isp will simply not be enough no matter what chemical combination that is used to warrant their use...
For really deep space missions with unmanned spacecraft, a proven upperstage like a Centaur is really tough to beat. For manned missions, you are going to need somekind of nuclear thermal rocket or VASIMR. The Isp penalty for an all chemical engine is just too large to make a manned mission practical for anything longer than near earth space. A near earth orbit crossins asteroid rendezvous is just about the limit for a manned and chemical propelled mission. The huge orbital fleets of the pre-Apollo, Von Braun era for a Mars mission are just too huge.
Welcome Big Brother. Some interesting posts and I'd like to ask a few additional questions.
Do you know what company is the prime contractor for the TR-3?
Same for the SR-3? (perhaps a different company for the vox?)
What ever happen to the Aurora project? Is that the same as the Darkstar or what?
Also, do you know anything about a tactical aircraft with reversed variable swept wings known at the "jackknife"? I saw something about that in some publication a few years back. I sometimes wonder as I mentioned before if the government doesn't from time to time plant misleading stories in the open literature just to throw adversaries off balance and perhaps cause them to waste valuable resources countering a non-capability. Then again sometimes these stories turn out to be very true as in the case of the F-19 except they had the designation wrong, i.e. F-117.
In my experience, rabbit trails and wild goose chases are less created by "planted" government stories, but more due to these actual scenarios:
1. Prototypes of systems employing new technologies are specified by DARPA, bid, then ordered; finally built by Northrop-Gruman, Boeing and Lockheed-Martin, tested thoroughly; and sad to say, some are then shelved for decades. Someone touring a base, such as Beale AFB sees a partially open hangar with a crescent-shaped craft and is told, "That doesn't exist, you didn't see that!" Just beacuse it never went into full production doesn't mean one or two don't exist. In 1996, their were probably only two AC-X (C-130) Laser Platforms. For example, some artist renditions show a red laser blasting the ground from the C-130, instead of blue. This is due mostly to a lack of first-hand experience of the artist. Their reference may have been the 747 laser color and made the wrong assumption.
2. Full-scale props are occasionally designed and constructed for sci-fi movie films, by private companies, covered during transport to maintain secrecy, and some photos or sketches are leaked.
On manufacturers, for SR-3 and TR-3, I can't say who built them. However, I relate who did not: Garrett Air Research/Allied Signal/Honeywell was suddenly ordered to lock files on a similar (though shorter) Navy stealth, the A-12.
What government officials are instructed to do is not discuss classified data. The PIO (public information officer or media press staff liaison) is given a cover story to hide the actual story from attracting further investigative research. Crashes of commercial aircraft are not immuned: TWA 800 & American 587. Because the cover stories were so obviously not followed up - no attempt by gov't of even pretending to go through the motions of grounding other identical planes with
As far as the other project names you mention, the challenge is like driving across town in some cities, where every so many miles the name of the street you are on changes. Remember the earlier names prior to F-19 "Have Blue?" And how the design morphed a bit, as the name changed? Same with the other programs. But, "Falcon" is indeed the current hypersonic aircraft name...
...(oops - Sorry, for the cut-off sentence above) Unfortunately, because government employees are instructed not to talk about certain events or projects, the incomplete record or untrue cover story remains in place, eyewitnesses are laughed at or attempts are made by unwitting PIO's to discredit them, and so it appears as though the government lies more than often than it does. That does not excuse those who do.
My FOIA request I made through Senator John McCain's office here c.1999-2000 did not result in any records on the B-70-like airframe I requested (we now know as the SR-3). Yet, I was sent fascinating declassified papers on a continuously manned nuclear-powered orbital bomber program 40-50 years old. Small nuclear reactors were constructed in order to power these crafts to stay aloft for years at a time. After studying the documents in detail, I feel the naysayers are without faith, rather than the CAMEL program to be a myth
Evidence is growing for a few classified space missions to other stars in our neighborhood, such as one craft leaving Earth's orbit & tracked heading toward Mu Cassiopeia in 1989. Laser communications from the space craft will be delayed for more than 20 years, once it approaches the binary systems of Mu and Eta Cassiopeia.
Northrop Grumman Designs Tailless Supersonic Aircraft With Darpa, AFRL
Aviation Week & Space Technology, 10/08/2007, page 56
Guy Norris, Los Angeles
Northrop Grumman is working aggressively to develop viable long-range supersonic-capable strike and reconnaissance aircraft, with a focus on two complementary tailless designs: an oblique flying wing (OFW), and a supersonic tailless air vehicle (STAV).
In development under a March 2006 Defense Advanced Research Projects Agency (Darpa) contract, the OFW is a twin-engined, supersonic flying wing that can vary the sweep angle for the most efficient flight performance. Now undergoing high-speed wind tunnel tests at Calspan in New York, the OFW is configured with "inlaid" control surfaces in lieu of vertical rudders or split-drag trailing edge rudders like the B-2.
The programs goal is to design and conduct flight tests of an experimental tailless, supersonic, variable-sweep flying wingand to demonstrate the feasibility of the concept for rapid deployment, long-range strike and long-endurance reconnaissance roles. At low speeds, the wing sweep is relatively low, providing an efficient aerodynamic design. At faster speeds, the wing is highly swept, reducing supersonic wave drag. Overall sweep for the current design is around 65 deg. at Mach 1.2, resulting in leading edge sweep angles of about 75 deg. for the trailing wing.
The first phase, which covers risk reduction of the critical technologies, has been extended to March 2008. Pending good results, a second phase is planned leading to construction of an experimental "X-plane" for first flight as early as 2010.
The companys tailless STAV project with the Air Force Research Laboratory (AFRL) has now transitioned to a follow-on STAV-systems integration (STAVSI) phase which is due to be completed in January 2008. "Were looking at the detailed integration of a preferred control system for a Mach 2.2 LRS system," says STAV Program Manager Steve Komadina.
Tracing its roots to studies with AFRL and the Aeronautical Systems Center at Wright-Patterson AFB, Ohio, STAV is aimed at lowering the weight and drag of traditional supersonic aircraft designs by replacing the conventional tail control surfaces with "innovative control effectors," says AFRL. These are thought to include a variety of potential options ranging from fluidic thrust vectoring, elevons and pitch flaps to spoiler slot deflectors, differential flaps and inlaid surfaces.
"We aimed at Mach 2 which looked like a sweet spot to us, and we looked at tailless supersonics and asked ourselves is that possible? Its turning out that we think it is," says Komadina. Next study phases are expected to include integrated power and thermal management systems as well as aeroelastic properties.
Assuming continued funding and positive test results, the goal is to build and fly a demonstrator around 2015. The timing would allow the advanced concept to slot into the U.S. Air Forces long-term plan to develop and field an advanced Phase 3 bomber for 2025 and beyond.
Aviation Week & Space Technology, 10/08/2007, page 34
Guy Norris, Los Angeles
Wind tunnel results point way forward for tailless oblique flying wing study
Prospects for the go-ahead of an ambitious oblique flying wing (OFW) "X-plane" supersonic demonstrator appear to have been boosted by completion of wind tunnel tests that, according to Northrop Grumman officials, prove the design is both workable and "robust."
The tests were conducted at various sweep angles from 0 to 65 deg. at speeds of Mach 0.4 to 1.3, on a 9% model at Calspans Buffalo, N.Y., site, and completed on Oct. 2. "It is the ultimate morphing aircraft," says Northrop Grumman OFW Program Manager Joe Pawlowski, adding that the data analysis will culminate with a preliminary design review (PDR) in March 2008 (see p. 56).
The PDR, if successful, will lay the foundations for a second phase that includes developing a flying demonstrator around 2010. The X-plane OFW will have a 56-ft. wing span, tricycle gear with an aft-mounted undercarriage leg, twin General Electric J85 afterburning turbojets and a sophisticated flight control system (FCS). With an aspect ratio of 7:1, the wing varies from 11% thickness at the center to 4% at the tips, and is designed to a demonstration point of Mach 1.2 with a 65-deg. sweep.
The J85s were selected because of a "good thrust-to-weight ratio, good fineness ratio and a nacelle pod with low supersonic drag," says OFW chief engineer Gary Tiebens.
Although originally paired close together, the predicted supersonic drag rise forced Northrop Grumman to move them apart for better area ruling. The engines pivot on a planetary gear system to follow line-of-flight commands from the FCS, says Tiebens, adding that they are not mechanically linked to one another.
Aimed at proving the concept of a supersonic, variable sweep, tailless aircraft, the OFW seeks to demonstrate the theoretical benefits of a configuration that increases sweep as speed grows. This increasing sweep enables the wing leading edge to stay behind the shock waves that form at the boundary between regions of subsonic and supersonic flow over the aircraft. Shock waves cause a form of drag known as wave drag, and merge to create pressure waves.
As a result, "the normal component of the wing stays subsonic, and never sees the increase in drag, and wont be littered by bunches of shocks," says Tiebens. "Its not an easy one to solve, and it has been one of the major design challenges, but we think weve tamed the beast and come up with a design that has been verified in the wind tunnel during these pre-tests."
The OFW unmanned air vehicle would sweep to 65 deg. for Mach 1.2 cruise speeds, but reduce to lesser angles for long-endurance loiter.Credit: NORTHROP GRUMMAN CONCEPT
The key test, however, was to prove that the low-drag configuration was also controllable. Although wave drag is reduced by the configuration, the center of pressure still moves aft with acceleration to supersonic speeds, causing pitch moment changes. In conventional designs this has been challenging to control, but with a flying wing without vertical tails the problems reach new levels, says Tiebens. "The vehicle is coupled in all three axesspanwise, vertical and longitudinal. If you make a pitch command on a [Boeing] 747 it only alters the pitch. In this, a pitch command also affects roll and yaw. Thats the Achilles heel of this configuration."
A dynamic flight simulation tool was developed to help perfect FCS algorithms that could control the aeroservo-elastic properties of the design and its "flexible aerodynamics," says Pawlowski. "Every time we change sweep its like a whole new aircraft." The FCS from the flexible aerodynamic modeling was combined with predictions from computational fluid dynamics work, and superimposed on the rigid body data collected in the wind tunnel.
The wing sports eight flight control surfaces, six on the trailing edge and two tip-mounted "inlaid" surfaces that are evolved from flight controls on the X-47 Pegasus unmanned air vehicle. The effect of the inlaid surfaces "varies with angle relative to oncoming flow," says Tiebens. "It is drag-producing, but there are side forces as well," he adds. The remaining surfaces act as ailerons while those i
FYI: Five years after the Phoenix Lights of March 1997, a smaller boomerang flying wing version chased semi's and cars which were driving along Interstate 10, at the Gila River, South of Phoenix.
Notice how much longer the triangular airframe seen flying over New Mexico is, (in proportion to its wingspan), below, than the canceled Navy A-12, above.
Fair Question. Where would you like the focus to be? SDI /Star Wars systems?
Let's start with alternate space ports and launches, and some early ground-based laser weapons adaptaions fro a-sat and anti-mines. [The next generation Humvee laser weapon being worked on currently is many times more powerful]: