No grāmatas satura
1.5. rezultāts no 98.
54. lappuse
... Propellant Supply Module , and the Thermal Control System components . Development tests of the Reaction Control System , ML 71-5241 , were conducted at the White Sands Test Facility and com- pleted in 1970. Verification tests will be ...
... Propellant Supply Module , and the Thermal Control System components . Development tests of the Reaction Control System , ML 71-5241 , were conducted at the White Sands Test Facility and com- pleted in 1970. Verification tests will be ...
63. lappuse
... propellants . Initially the shuttle will be used to orbit and retrieve automated satellites , MH 71-5233 . The Space Sciences and Applications Office of NASA has many missions for future shuttle flights already identified . These ...
... propellants . Initially the shuttle will be used to orbit and retrieve automated satellites , MH 71-5233 . The Space Sciences and Applications Office of NASA has many missions for future shuttle flights already identified . These ...
64. lappuse
... DURATION SCIENCE AND APPLICATIONS MISSIONS RESEARCH LABORATORY SPACE RESCUE PROPELLANT DELIVERY SPACE STATION SUPPORT NASA HQ MH71-5179 REV 2-23-71 SPACE SHUTTLE PROPOSED LEADING EDGE WING SECTION GENERAL DYNAMICS Convair. 64.
... DURATION SCIENCE AND APPLICATIONS MISSIONS RESEARCH LABORATORY SPACE RESCUE PROPELLANT DELIVERY SPACE STATION SUPPORT NASA HQ MH71-5179 REV 2-23-71 SPACE SHUTTLE PROPOSED LEADING EDGE WING SECTION GENERAL DYNAMICS Convair. 64.
77. lappuse
... propellant mixture ratio control ; throttleability ; minimum maintenance . The engine will not represent a modification of existing engines , but will be of new design based on technology concepts developed during the 1960s . This is ...
... propellant mixture ratio control ; throttleability ; minimum maintenance . The engine will not represent a modification of existing engines , but will be of new design based on technology concepts developed during the 1960s . This is ...
78. lappuse
... propellant flow diagram of one of these engines , MH 71-5102 . Propel- lant flow paths only are illustrated in this diagram as the fuel and oxidizer are shown proceeding through two pumping stages to achieve the necessary high injection ...
... propellant flow diagram of one of these engines , MH 71-5102 . Propel- lant flow paths only are illustrated in this diagram as the fuel and oxidizer are shown proceeding through two pumping stages to achieve the necessary high injection ...
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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