ROCKET

RAND's Omnibus Calculator of the Kinematics of Earth Trajectories

by Barry W. Boehm

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A reference manual for the ROCKET program, which mathematically simulates the flight of aerospace vehicles by means of a digital computer. The program is versatile and easily mastered and has been used to study the following: space booster performance, hard-point defense, satellite rendezvous, ballistic missile performance, satellite orbit decay, verification of aerodynamic characteristics, maneuverability, reentry phenomena, evaluation of rocket vehicle guidance, and lunar and planetary exploration.

This report is part of the RAND Corporation Research memorandum series. The Research Memorandum was a product of the RAND Corporation from 1948 to 1973 that represented working papers meant to report current results of RAND research to appropriate audiences.

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