Aeronautics and astronautics – Spacecraft – Attitude control
Patent
1990-09-11
1992-10-27
Peters, Jr., Joseph F.
Aeronautics and astronautics
Spacecraft
Attitude control
244161, B64G 162
Patent
active
051582481
ABSTRACT:
A re-entry vehicle that includes three detachable modular components which anticipate total re-useability. Modularization of the composite re-entry vehicle offers great flexibility in re-arranging the various modules to suit a particular mission. The three module components include a crew module, principally serving as a crew cabin, and attached thereto is a modular heat shield or re-entry module which principally provides for thermal protection of the cabin module during re-entry. Propulsion for the cabin module to achieve a particular re-entry orbit is provided by a versatile service stage which becomes detached from the other two modules upon attainment of a desired re-entry trajectory. When used in conjunction with a Space Station, the versatile service stage may be propelled back to the Space Station for refueling and re-use.
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Grumman Aerospace Corporation
Mojica Virna Lissi
Peters Jr. Joseph F.
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