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THE UNKNOWN COSMOS 201
FLIGHT PERFORMANCE OF A ROCKET
TRAJECTORY OPTIMIZATION FOR POWERED FLIGHT
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acceleration accelerometer aerodynamic altitude analysis angle antenna approximately atmosphere axis ballistic vehicle cent chamber circular orbit combustion components computed constant curve deceleration density departure direction distance drag earth earth's atmosphere effect ellipse energy engine equation error escape exhaust velocity factor field Figure flight flow force frequency ft/sec fuel function gimbal given gravitational guidance gyro heat transfer heliocentric hyperbolic increase inertial initial integral interplanetary liquid lunar Mars mass flow rate maximum measured miles missile mission moon motion nautical miles neutron nodal line nozzle obtained optimum parameter payload periapsis perigee perturbations planet pressure problem propulsion system radiation radius range reactor reference relative result satellite orbit semimajor axis shown in Fig signal solar system solid propellant space vehicle specific impulse stagnation point structure surface tank target temperature thrust tion torque trajectory transfer orbit true anomaly turbopump vector weight zero