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DESIGN STATUS OF COMMAND AND SERVICE MODULESby R L Benner North American Aviation
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SIMULATION OF A MINIMUM VARIANCE ORBITAL NAVIGATION SYSTEMby James L Farrell Westinghouse
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acceleration airbreathing aircraft analysis angle angular Apollo approximately astronaut attitude control base boost cabin capability capsule carbon dioxide command components concept configuration control system cost covariance matrix crew cryogenic display docking Earth effect engine entry equations equipment error flight fuel cell function Gemini Gemini program guidance heat impact initial landing launch weight load loop lunar surface maneuver Mars maximum ment meteoroid minimum mission mode module NASA nautical miles navigation operation orbit oxygen parameters partial pressure payload performance phase pilot position pounds pressure problem propellant propulsion radiator range re-entry rendezvous reticle reusable rocket sensor shock absorber shown in Figure simulation space station space suit spacecraft specific impulse stage structure subsystem swingby target technique temperature thermal thrust thrust vector tion trajectory transfer utilized valve vector vehicle velocity vertical zero