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Operational Requirements for Large Space
Logistics Tomorrow Support in Space
16 other sections not shown
acceleration accuracy Aerospace aircraft analog computer angular angular velocity approximately ascent assembly attitude axes axis basic Bell Aerosystems booster cables capability center of mass checkout complete components concept control system coordinate cost determine effects Engineering environment equations error evaluation factors failure Figure fixed flight functions gravity guidance hardware helicopter helium human human reliability impact-point inertial initial injection inputs launch point launch time tolerance lunar maintenance maneuver measurements ment method milliseconds minimum missile mission moon's orbital plane obtained operational orbital element orbital worker orbital-element output panel parameters parking orbit performance platform Polaris missiles problem procedure propellant radar range angle reliability rotation signal simulation space vehicle specific storage Subroutine subsystem support equipment tank techniques telemetry temperature terminal test equipment test point design thrust thrust vector tion torque tracking trainer translation translunar trajectory UDMH utilized values vector weight weightlessness