Results of first phase of program to define resistojet control system for manned orbiting research laboratory (MORL); 10-mib hydrogen ammonia, and biowaste thruster systems are defined to satisfy impulse requirements arising from aerodynamic and gravity-gradient forces in orbit; of available biowastes (H2, Co2 and fecal water), CO2 output alone was sufficient to provide impulse requirements for 10-mlb system; however, combined CO2/H2 system permits greater growth capability at expense of simplicity; use of resistojet thruster system to provide orbit injection and high-disturbance control impulse was also investigated.


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    Title :

    Subsystems analyses for MORL resistojet control system


    Additional title:

    J Spacecraft Rockets


    Contributors:

    Published in:

    Publication date :

    1968


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :