Members Login
Username 
 
Password 
    Remember Me  
Post Info TOPIC: Atlas V launch
10kBq jaro

Date:
Atlas V launch


some interesting photos of solid booster sep....


Space Technology


Most Powerful Atlas V to Date Launches Inmarsat 4


Aviation Week & Space Technology


03/28/2005, page 58


Craig Covault


Cape Canaveral


Inmarsat's business propelled to new heights by extra Aerojet solid motors on Atlas V


Heaviest Satcom


The first EADS/Astrium Inmarsat 4, the largest commercial communications satellite ever launched, has completed four maneuvers to reach geosynchronous orbit where it has deployed its 30 X 40-ft. elliptical reflector and solar arrays spanning 148 ft.


Inmarsat 4 is being parked temporarily at a test location near the west coast of Africa before being drifted by late May toward its operational mobile communications station at 64 deg. E. Long. over the Indian Ocean.


The 13,183-lb. spacecraft was launched Mar. 11 from Cape Canaveral on the most powerful version to date of the Lockheed Martin International Launch Services (ILS) Atlas V.


The Inmarsat 4 spacecraft, with 630 channels and 228 spot beams, is the most complex civilian communications spacecraft ever built, says Michel LeMoine, EADS/Astrium Inmarsat 4 program director (AW&ST Mar. 7, p. 36).


The second Inmarsat 4 is to be parked later this year over the Atlantic region following launch on a Sea Launch Zenit. A third will later be placed over the Pacific region using a launcher yet to be selected.


The combined cost of the spacecraft and ILS mission was at least $250 million. And ILS and Inmarsat integrated Inmarsat 4 engineering details for five years before the flight, says Mike Jensen, ILS vice president for technical operations.


The Atlas V/431 vehicle--using three Aerojet solid motors (SRMs), a Russian Energomash/Pratt & Whitney RD-180 engine, and single-engine Pratt RL10 Centaur--put Inmarsat 4 into an initial 56,270 X 274-mi. "supersynchronous" transfer orbit.


The spacecraft's initial apogee, extending a quarter of the distance between the Earth and the Moon, was more than double the normal altitude used for satcom transfer orbits.


Inmarsat and Astrium calculated that by launching to a higher initial orbit, before maneuvering to about 22,300 mi., the spacecraft could conserve propellant to operate until at least 2020, says Andrew Sukawaty, Inmarsat CEO/chairman.


Inmarsat controllers commanded the satellite through four burns to raise perigee and lower apogee to the 22,300-mi. operational altitude at 0 deg. inclination.


http://www.aviationnow.com/media/images/awst_images/large/AW_03_28_2005_1306_L.jpg The most powerful Atlas V flown to date lifts off on 1.76 million lb. thrust with Inmarsat 4, the heaviest commercial satcom ever flown.Credit: LOCKHEED MARTIN


The spacecraft was assembled at Astrium facilities in the U.K., Germany, Spain and France, and about 150 European managers and engineers attended the launch. Their presence, along with the standard complement of Russian RD-180 engineers, exercised the Atlas Space Operations Center (ASOC) provisions for International Traffic in Arms (ITAR) regulations.


The Russians were positioned in an ASOC Mission Support Room with computer access to RD-180 system displays only, while the European managers and guests were restricted to a specific ASOC area where they could see just the U.S. system displays allowed with a special electronically programmed access card.


The Atlas V for the first time used three Aerojet SRMs instead of the twin solid motor configuration used earlier. Two of the 300,000-lb.-thrust SRMs were on one side of the vehicle and the third on the opposite side, a unique asymmetrical configuration.


The 194-ft.-tall vehicle weighed more than 1 million lb. on its Launch Complex 41 mobile launcher platform. This included 51 tons for each of the three SRMs. The vehicle lifted off on 1.76 million lb. thrust, with 900,000 lb. of that contributed by the three Aerojet solid motors and 860,000 lb. from the RD-180 operating at 100% throttle.


The twin rocket nozzles of the RD-180 were canted 0.4 deg. off center at liftoff to counter the extra 51 tons of mass on the side of the vehicle with the second SRM. The RD-180's throttling capability was used extensively during the ascent to maintain vehicle dynamic load limits in connection with the extra power from the solid motors.


http://www.aviationnow.com/media/images/awst_images/large/AW_03_28_2005_1307_L.jpg The Atlas V first-stage camera shows separation of two of the three Aerojet 300,000-lb.-thrust solid motors at 27 mi. altitude. Note Cape Canaveral on the ground below and Earth's horizon at top. The next Atlas V, with no solids, will launch the Mars Reconnaissance Orbiter in August. The Pluto mission Atlas V in 2006 will have five solids.Credit: LOCKHEED MARTIN COMMUNICATIONS


At 10 sec. after clearing the mobile launcher platform, the RD-180 was throttled down to 87% thrust and the Aerojet motors continued to provide 900,000 lb. thrust.


Then at 12 sec., the RD-180 was throttled down further to 60.7% to slow the rate of acceleration as the vehicle went supersonic, experiencing the highest dynamic loads of the flight--Max-Q.


After Max-Q, the RD-180 was throttled back up to 64% thrust.


The Aerojet solids burned out as intended at 91 sec., followed immediately by the RD-180 being throttled back up to 100% and generating 933,000 lb. of thrust in a vacuum. The depleted SRMs, down to 4 tons each, were separated 38 sec. after burnout, with the vehicle at 27 mi. altitude.


The Atlas V then shifted to closed-loop guidance, where it continually updated its own thrust and steering commands to achieve precise velocity and altitude cutoff targets. The RD-180 throttled down in three more steps before first-stage burnout at 60 mi. altitude and 11,000 mph.


The oxygen/hydrogen RL10 engine Centaur then ignited with 22,300 lb. thrust for a nearly 10-min. firing to accelerate the vehicle to 17,500 mph., placing it in a low parking orbit for a 10-min. coast across the Atlantic.


http://www.aviationnow.com/media/images/awst_images/large/AW_03_28_2005_1308_L.jpg The Atlas V first-stage camera shows separation of two of the three Aerojet 300,000-lb.-thrust solid motors at 27 mi. altitude. Note Cape Canaveral on the ground below and Earth's horizon at top. The next Atlas V, with no solids, will launch the Mars Reconnaissance Orbiter in August. The Pluto mission Atlas V in 2006 will have five solids.Credit: LOCKHEED MARTIN COMMUNICATIONS


Just off the west coast of Africa, the Pratt RL10 was ignited again to place the spacecraft in the transfer orbit where the stage imparted a 2.5-deg.-per-sec. spin rate before separation over south central Africa 32 min. after launch.



__________________
Page 1 of 1  sorted by
 
Quick Reply

Please log in to post quick replies.

Tweet this page Post to Digg Post to Del.icio.us


Create your own FREE Forum
Report Abuse
Powered by ActiveBoard