Unmanned craft

Aeronautics and astronautics – Aircraft propulsion – Launching

Patent

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Details

89 1801, 89 1816, 89 1819, 244 14, 244 327, 244 49, 244120, B64F 104, F41F 300

Patent

active

044101511

ABSTRACT:
A vehicle or craft is provided for propeller propulsion with start assist by a releasable rocket engine. The craft is launched from a silo of square-shaped cross-section containing the starter motor for the propeller, whose engine is started while the craft is still in the silo. Diagonally opposed corners of the silo are provided with rails, in which run guides on rudder fins of the craft. The wings are pivoted to the fuselage for deployment whereby the wing tips do not move forward. The rocket engine is jettisoned shortly after take-off by simple disengagement. Parts of the wings and/or the rear of the fuselage may be jettisoned shortly before the craft reaches the target area.

REFERENCES:
patent: 2375423 (1945-05-01), Lobelle
patent: 2390677 (1945-12-01), Alkan et al.
patent: 2748703 (1956-06-01), Goss et al.
patent: 2961928 (1960-11-01), Rosenthal
patent: 2992794 (1961-07-01), Boyd
patent: 3063375 (1962-11-01), Hawley et al.
patent: 3132590 (1964-05-01), Hall
patent: 3138352 (1964-06-01), Saholt
patent: 3460430 (1969-08-01), Fisher
patent: 3769876 (1973-11-01), Haas et al.
patent: 3988206 (1976-11-01), Gregory
patent: 4296894 (1981-10-01), Schnabele et al.
Jane's All the World Aircraft, 1977-1978, pp. 643-644, "Canadair CL-89".
Rockwell International, "Forward Swept Wing Technology", 1979.

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