Winged spacecraft

Aeronautics and astronautics – Spacecraft – Reusable or returnable

Reexamination Certificate

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Reexamination Certificate

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10515777

ABSTRACT:
A rocket-powered spacecraft having a wing which has hinged aft portions which can be elevated about a hinge line. Tail booms extend rearwardly from the outer ends of the aft wing portions, and rudders are mounted at the aft ends of the booms. Each tail boom supports a horizontal tail with an elevon at its trailing edge. In normal flight, the wing aft portions are not elevated, and the wing has a normal airfoil shape. During atmosphere reentry, the wing aft portions are steeply elevated to provide a stable high-drag altitude for the spaceship for speed reduction at low thermal and structural loading. After reentry, the aft wing is returned to an unelevated position which enables gliding flight to a horizontal-runway landing.

REFERENCES:
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patent: 3125313 (1964-03-01), Soderberg
patent: 3160366 (1964-12-01), Graffenried
patent: 3204892 (1965-09-01), Powell
patent: RE26380 (1968-04-01), Rogallo
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patent: 5029773 (1991-07-01), Lecat
patent: 5169095 (1992-12-01), Lecat
patent: 6502785 (2003-01-01), Teter et al.
patent: 03167098 (1991-07-01), None
Abstract of Japanese Patent No. JP 403167098 A, Published Jul. 18, 1991, Inventor Horikawa, Makoto.

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