Proceedings, Volume 11967 |
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Page 145
THE INTEGRATED TELEMETRY AND CHECKOUT SYSTEM OF THE OPERATIONAL ELDO - A THIRD STAGE by H. REIMANN Bölkow GmbH , Ottobrunn bei München ( GFR ) The present ELDO - A vehicle uses different telemetry and checkout systems for the different ...
THE INTEGRATED TELEMETRY AND CHECKOUT SYSTEM OF THE OPERATIONAL ELDO - A THIRD STAGE by H. REIMANN Bölkow GmbH , Ottobrunn bei München ( GFR ) The present ELDO - A vehicle uses different telemetry and checkout systems for the different ...
Page 295
... checkout of the Uprated Saturn I and Saturn V space vehicle programs and still allow manual control of the check- out process . A two - computer system was selected by National Aeronautics and Space Administration , and the ...
... checkout of the Uprated Saturn I and Saturn V space vehicle programs and still allow manual control of the check- out process . A two - computer system was selected by National Aeronautics and Space Administration , and the ...
Page 301
propellant subsystems , electronic onboard subsystems , gyro subsystems , and flight control subsystem checkout . The constant programmer - engineer interface needed for automation definition , in addition to the complexity of the checkout ...
propellant subsystems , electronic onboard subsystems , gyro subsystems , and flight control subsystem checkout . The constant programmer - engineer interface needed for automation definition , in addition to the complexity of the checkout ...
Contents
W NASA Washington D C U S A 53 555 | 3 |
A Review of the Gemini Manned Spaceflight Program Survey Paper G | 55 |
Apollo Lunar Surface Experiment Package ALSEP D Bitondo | 83 |
Copyright | |
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Agena Agena target vehicle ALSEP analysis antenna Apollo approximately astronaut attitude control battery checkout circuit command COMPARTMENT components composite materials configuration control system crew deux devices Earth electrical electronic elements engine environment equipment étage été experiments flight fonctionnement Gemini Gemini IX Gemini Program Gemini VII Gemini XI gravity gradient Hawker Siddeley Dynamics heat transfer heater initial insulation integrated integrated circuits l'ensemble l'équateur laboratory lanceur launch vehicle le satellite loading Lunar Orbiter lunar surface magnetic magnetometer maneuver Mariner Mars material mise mission module n.mi NASA nodal node on-board operation payload performance périgée phase phase-locked loop plate problems propellant propulsion radiation reflector reliability rendezvous rotation S-IVB satellite Saturn scientific sensor shown in Fig space spacecraft spin axis stabilization stage stiffness stress structure subsystem tank techniques telemetry thermal control thermocouple tion vector velocity vitesse weight wire