No grāmatas satura
1.–5. rezultāts no 100.
59. lappuse
... engine and one for the vehicle itself . These con- tracts are well underway and what is beginning to emerge is a ... engine that can be used on both the orbiter and the booster . Engines , as you know have historically been the longest ...
... engine and one for the vehicle itself . These con- tracts are well underway and what is beginning to emerge is a ... engine that can be used on both the orbiter and the booster . Engines , as you know have historically been the longest ...
60. lappuse
... engine . Basic objectives are to define the Shuttle system and the engine requirements , accomplish prelimin- ary design , and predict the scope , schedule and cost of a fully reusable two stage shuttle . Meanwhile other contractual ...
... engine . Basic objectives are to define the Shuttle system and the engine requirements , accomplish prelimin- ary design , and predict the scope , schedule and cost of a fully reusable two stage shuttle . Meanwhile other contractual ...
61. lappuse
... ENGINE BASELINED AT 550,000 POUNDS SEA LEVEL THRUST ( BOOSTER AND ORBITER ) • AIR BREATHING ENGINES USE JET FUEL • ACCELERATION NOT TO EXCEED 3 G's NASA HQ MH71-5390 3-1-71 TYPICAL SPACE SHUTTLE INBOARD PROFILE - ORBITER ON ORBIT ENGINES ...
... ENGINE BASELINED AT 550,000 POUNDS SEA LEVEL THRUST ( BOOSTER AND ORBITER ) • AIR BREATHING ENGINES USE JET FUEL • ACCELERATION NOT TO EXCEED 3 G's NASA HQ MH71-5390 3-1-71 TYPICAL SPACE SHUTTLE INBOARD PROFILE - ORBITER ON ORBIT ENGINES ...
69. lappuse
... engine efforts will include development testing of the thrust chamber and engine controls , and design of a prototype engine . Propulsion subsystem test facilities will be modified and development hardware tested . Fabrication of a ...
... engine efforts will include development testing of the thrust chamber and engine controls , and design of a prototype engine . Propulsion subsystem test facilities will be modified and development hardware tested . Fabrication of a ...
70. lappuse
... engine concept . Vehicle ( Orbiter and Booster ) and engine parametric studies were completed in 1970. The prototype engine design review , the design and development plan , and the final engine definition studies review will be ...
... engine concept . Vehicle ( Orbiter and Booster ) and engine parametric studies were completed in 1970. The prototype engine design review , the design and development plan , and the final engine definition studies review will be ...
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activities Aerojet aerospace AIRLOCK analysis Apollo 15 Apollo program Apollo Telescope Mount applications ASSEMBLY astronauts Boeing booster capability chamber chart checkout combustion components concept configuration contract contractors Convair cost crew earth orbit Earth Resources environment equipment evaluation facilities FIGURE function future going hardware heat injector integrated Kennedy Space Center laboratory landing launch vehicle lunar major manufacturing materials MCDONNELL DOUGLAS ment million mission MSFC NASA HQ North American Rockwell operations ORBITAL WORKSHOP payload performance phase planning preburner problems propellant propulsion reduce requirements reusable rocket S-IVB satellites Saturn IB schedule SCIENCE scientific Service Module shown SKYLAB EXPERIMENT Skylab Program SLIDE solar Space Flight space program SPACE SHUTTLE PROGRAM Space Station spacecraft stage structure studies subsystems surface tanks TEAGUE technical Telescope thermal protection system thrust tion transportation turbopumps unmanned utilization weight