No grāmatas satura
1.–5. rezultāts no 100.
2071. lappuse
... earth - to - orbit and earth - to - earth trans- portation system is illustrated in the next chart , figure 182 , page 2087. The first- stage booster is a HTOHL hypersonic - cruise airplane with turboramjet air- breathing propulsion ...
... earth - to - orbit and earth - to - earth trans- portation system is illustrated in the next chart , figure 182 , page 2087. The first- stage booster is a HTOHL hypersonic - cruise airplane with turboramjet air- breathing propulsion ...
2087. lappuse
... EARTH - TO - EARTH SPACE STATION 2ND STAGE ORBITAL SUPPLY 2ND STAGE EARTH - TO - EARTH NASA R63-1084 FIGURE 182 Mr. RANDALL . And what do you call it ? Mr. KARTH . Hypersonic transportation ? Mr. ZIMMERMAN . That's a good description ...
... EARTH - TO - EARTH SPACE STATION 2ND STAGE ORBITAL SUPPLY 2ND STAGE EARTH - TO - EARTH NASA R63-1084 FIGURE 182 Mr. RANDALL . And what do you call it ? Mr. KARTH . Hypersonic transportation ? Mr. ZIMMERMAN . That's a good description ...
2095. lappuse
... Earth - to - orbit and return transportation system for either military or NASA functions . ( b ) An Earth - to - Earth transportation system as supported by the technology for ( a ) for either military or commercial purposes . In order ...
... Earth - to - orbit and return transportation system for either military or NASA functions . ( b ) An Earth - to - Earth transportation system as supported by the technology for ( a ) for either military or commercial purposes . In order ...
2098. lappuse
... Earth based tracking and command systems to guide with reasonable accuracy as distances from Earth become great , and the desirability of having onboard naviga- tion capability for manned systems , indicate the establishment of a strong ...
... Earth based tracking and command systems to guide with reasonable accuracy as distances from Earth become great , and the desirability of having onboard naviga- tion capability for manned systems , indicate the establishment of a strong ...
2101. lappuse
... EARTH 362 DAYS MARS EARTH O DAYS SPIRAL MARS 139 DAYS COAST PERIOD 415 DAY MARS ORBITER MISSION ERROR ERROR ANALYSIS EFFECT CONCLUSION 22 LBS . IN VEHICLE WT . 200,000 MILE POSITION ERROR REPETITIVE TRAJECTORY 200,000 MILE POSITION ...
... EARTH 362 DAYS MARS EARTH O DAYS SPIRAL MARS 139 DAYS COAST PERIOD 415 DAY MARS ORBITER MISSION ERROR ERROR ANALYSIS EFFECT CONCLUSION 22 LBS . IN VEHICLE WT . 200,000 MILE POSITION ERROR REPETITIVE TRAJECTORY 200,000 MILE POSITION ...
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advanced research Air Force aircraft AMES analog computers antenna atmosphere BISPLINGHOFF budget Calif capabilities in electronics Chairman Colonel GOULD communications components control systems Corp data processing devices Division effort electrical electronics research engine environment equipment experiments facilities figure fiscal year 1964 fuel cell going guidance heat hypersonic industry instrumentation KARTH KELLEY KONECCI Langley Langley Research Center launch vehicles lunar materials meteoroid micrometeorites microwave million missions MORRIS MOSHER NASA NERVA nuclear OART Office operation optical orbit particles physics planetary problems propellant propulsion radar radiation radio RANDALL Ranger program reactor reentry requirements research and technology Research capabilities Research Center rocket satellite Saturn semiconductors simulation slide fig SLOOP solar solar cells solid solid state physics space flight Space Sciences space vehicles spacecraft structural studies subcommittee supersonic supersonic transport techniques temperature tion Titan III University V/STOL ZIMMERMAN