Aeronautics and astronautics – Spacecraft – Attitude control
Patent
1984-05-25
1987-01-13
Barefoot, Galen L.
Aeronautics and astronautics
Spacecraft
Attitude control
244 72, 60 39463, 60210, 60218, B64G 126
Patent
active
046358854
ABSTRACT:
Disclosed is a single control thruster having the expanded capability of operating at various thrust levels and more than one propellant fluid so that the number of control thrusters for a maneuvering vehicle can be reduced to one third from that now required for appropriate maneuverability in space, resulting in large cost savings and improved reliability. Also disclosed is a "plug in" package with control thruster which can be removed from the vehicle and replaced to make the vehicle easily maintainable.
REFERENCES:
patent: 3097480 (1963-07-01), John
patent: 3180084 (1965-04-01), Meeks
patent: 3358456 (1967-12-01), Lehrer
patent: 3446023 (1969-05-01), Mosier
patent: 3514953 (1970-06-01), Kephart
patent: 3673801 (1972-07-01), Goldberger
patent: 4490972 (1985-01-01), Ellian et al.
Barefoot Galen L.
Duncan John R.
General Dynamics Corporation/Convair Div.
Gilliam Frank D.
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