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MISSION ENVELOPE AND PLANNING
TASK PERFORMANCE ANALYSIS
GENERAL DESCRIPTION OF THE SERVICE VEHICLES
16 other sections not shown
adhesives altitude change analysis angle antenna astronaut attitude control bandwidth beryllium btu/hr cabin cabin pressure calculated CHAPTER circular orbit communication components configuration continuous cluster cost crew deadband developed earth effect electrical energy Engineering environment Equation equipment factor fluid Freon frequency ft/sec fuel cell function half hard suit heat transfer Hohmann transfer intermittent cluster limit cycle liquid loads lubricants maneuvers manipulators material maximum meteoroid micrometeoroids minimum mission module nodal regression noise temperature nuclear operation orbital periods oxygen parameters perigee power system pressure propellant propulsion system psia pulse radar radiator range ratio refurbishment rendezvous robot SSV rocket satellite selection service vehicle shown in Figure solar space station spacecraft specific impulse structural subsystems surface Table task performance telemetry television terminal phase thermal control thrust thrusters tubes University of Houston unmanned vehicle vacuum velocity weight