Launch Vehicles - Boeing Delta III PERFORM AN CE Maximum...

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Unformatted text preview: Boeing Delta III PERFORM AN CE Maximum Speed W E IG H T S Payload for Low Earth Orbit D E S IG N S T A N D A R D S Zero Stage Engines: E X T E R IO R Height 135 ft 13 ft Payload Diameter nine Alliant (solid) 97,000 lb thrust each 90 sec burn 37,000 lb HTPB each 265 sec burn 18,280 lb CO Another motor on payload over 17,000 mph burning tank Payload for Geosynchronous Transfer Orbit 8,400 lb Oxygen tank First Stage Engine: Rocketdyne RS27A 165,000 lb thrust 64,000 lb kerosene 144, 000 lb oxygen Pratt & Whitney RL10B2 22,000 lb thrust 525 sec burn 4,000 lb hydrogen 22,000 lb oxygen Kerosene tank Second Stage Engine: RS-27A main engine PERF ORM AN C E Orbital Sciences Pegasus XL Maximum Speed W EIGH TS Payload for Geosynchronous Transfer Orbit D ESIGN STAN D ARD S First Stage Engine: Secomd Stage Engine: Third Stage Engine: EXTERIOR Length Diameter Wingspan 685.4 in 50 in 264 in Orion 50S XL Orion 50 XL Orion 38 18,000 mph 500 lb 163,000 lb 44,000 lb 8,000 lb Pegasus XL Mission Profile to 400 nm Circular, Polar Orbit with a 501 lb Payload ...
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This note was uploaded on 09/21/2008 for the course ASE 1013 taught by Professor Koenig during the Fall '07 term at Mississippi State.

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Launch Vehicles - Boeing Delta III PERFORM AN CE Maximum...

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