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    In:  CASI
    Publication Date: 2005-11-30
    Description: The accuracy of a direct contact method with a spacecraft to determine the mass of an orbiting object was studied. The precedure involved acceleration of the Gemini Agena target vehicle by the use of the Gemini 9 spacecraft propulsion system. The target vehicle mass was calculated from the resultant acceleration, updated Gemini spacecraft mass, and calibrated thrust levels of the air-firing thrusters of the orbital attitude and maneuver system of the Gemini spacecraft.
    Keywords: SPACE SCIENCES
    Type: The Gemini Program: Phys. Sci. Expt. Sum.; p 555-559
    Format: text
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