No grāmatas satura
1.–5. rezultāts no 100.
2. lappuse
... solar wind . We know that the crust of the moon has considerable strength because it is able to support immense mass concentrations at or near the surface in several of the Lunar " Seas " such as Imbrium . These mass concentrations were ...
... solar wind . We know that the crust of the moon has considerable strength because it is able to support immense mass concentrations at or near the surface in several of the Lunar " Seas " such as Imbrium . These mass concentrations were ...
9. lappuse
... solar system and galaxy . Photographs of the Descartes area were also taken to aid in the planning for the forthcoming Apollo 16 mission . It is obvious that Apollo 14 will be a very rewarding scientific mission . APOLLO 15 David R ...
... solar system and galaxy . Photographs of the Descartes area were also taken to aid in the planning for the forthcoming Apollo 16 mission . It is obvious that Apollo 14 will be a very rewarding scientific mission . APOLLO 15 David R ...
12. lappuse
... solar wind boundary layer over the Moon , monitor solar flare electron events , study the magnetic field interaction with the Moon and measure the particle flux in and near the plasma sheet . In addition the Module will include a ...
... solar wind boundary layer over the Moon , monitor solar flare electron events , study the magnetic field interaction with the Moon and measure the particle flux in and near the plasma sheet . In addition the Module will include a ...
15. lappuse
... solar arrays is 90 feet . The internal habitable volume is almost 13,000 cubic feet , comparable to a farily ample three bedroom house . The Skylab is made up of four major modules : The Workshop Module . The Airlock Module . The ...
... solar arrays is 90 feet . The internal habitable volume is almost 13,000 cubic feet , comparable to a farily ample three bedroom house . The Skylab is made up of four major modules : The Workshop Module . The Airlock Module . The ...
19. lappuse
... SOLAR EXPERIMENTS • CLUSTER ATTITUDE CONTROL • PRECISE SUN POINTING CONTROL ELECTRICAL POWER ( SOLAR ARRAYS ) TELEMETRY WITH GROUND DIMENSIONS 1. RACK : WIDTH 11 FT . HEIGHT 9 FT . 5 IN . 2. CANNISTER : DIA . 7 FT . HEIGHT 11FT . 3 ...
... SOLAR EXPERIMENTS • CLUSTER ATTITUDE CONTROL • PRECISE SUN POINTING CONTROL ELECTRICAL POWER ( SOLAR ARRAYS ) TELEMETRY WITH GROUND DIMENSIONS 1. RACK : WIDTH 11 FT . HEIGHT 9 FT . 5 IN . 2. CANNISTER : DIA . 7 FT . HEIGHT 11FT . 3 ...
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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