No grāmatas satura
1.–5. rezultāts no 100.
5. lappuse
... tank resulting in internal pressure which caused the tank to rupture . These wires were inadvertently damaged during pre - launch checkout at Cape Kennedy , although no evidence of the dam- aged wires was detected during the testing at ...
... tank resulting in internal pressure which caused the tank to rupture . These wires were inadvertently damaged during pre - launch checkout at Cape Kennedy , although no evidence of the dam- aged wires was detected during the testing at ...
6. lappuse
... tanks failed . Other modifications included removal of electric motors and fans from exposure to the high pres- sure oxygen atmosphere , changes in the tank wiring insulation , using stainless steel rather than aluminum quantity sensing ...
... tanks failed . Other modifications included removal of electric motors and fans from exposure to the high pres- sure oxygen atmosphere , changes in the tank wiring insulation , using stainless steel rather than aluminum quantity sensing ...
61. lappuse
... IV CENTAUR TURBOFAN ENGINES LH2 TANK PAYLOAD BAY 59-311 0-71 - No . 2 , pt . 2-5 LH 2 ON ORBIT TANKS MAIN ENGINES LO 2 TANKS NASA HQ MH71-5015 SPACE SHUTTLE CROSSRANGE UNCORECTED LANDING PATH 1100NM FROM ORBIT CROSSRANGE 1-6-71 61.
... IV CENTAUR TURBOFAN ENGINES LH2 TANK PAYLOAD BAY 59-311 0-71 - No . 2 , pt . 2-5 LH 2 ON ORBIT TANKS MAIN ENGINES LO 2 TANKS NASA HQ MH71-5015 SPACE SHUTTLE CROSSRANGE UNCORECTED LANDING PATH 1100NM FROM ORBIT CROSSRANGE 1-6-71 61.
70. lappuse
... tanks , and attachment mechanisms . Mission simulations will be performed in combination with thermal protection systems . Analysis and test of electrical subsystems and of many new alloys and promising materials are planned . A ...
... tanks , and attachment mechanisms . Mission simulations will be performed in combination with thermal protection systems . Analysis and test of electrical subsystems and of many new alloys and promising materials are planned . A ...
72. lappuse
... tanks for lower altitude multi - staging . A second type is called the drop tank configuration , which includes a fully reusable Booster and Orbiter with external hydrogen fuel tanks detachable from the Orbiter . These drop tanks would ...
... tanks for lower altitude multi - staging . A second type is called the drop tank configuration , which includes a fully reusable Booster and Orbiter with external hydrogen fuel tanks detachable from the Orbiter . These drop tanks would ...
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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