Republic SD-4 Swallow
The SD-4 Swallow supersonic reconnaissance drone was built in 1960 under a U.S. Army contract. The SD-4, which was to be part of the AN/USD-4 surveillance drone system, was a delta-wing design powered by a single Pratt & Whitney JT12A-3 turbojet. The Swallow was zero-length launched with the help of two solid-fueled rocket boosters, and could be recovered by parachute. Similar to Republic's earlier SD-3 Snooper drone, it had interchangeable nose sections for photographic, radar or infrared surveillance equipment.
Photo: Republic |
SD-4 |
The AN/USD-4 program was cancelled by the U.S. Army in January 1961, and it is not clear whether any SD-4 vehicles were actually test-flown.
Specifications
Note: Data given by several sources show slight variations. Figures given below may therefore be inaccurate!
Data for SD-4:
Length | 9.27 m (30 ft 5 in) |
Wingspan | 3.51 m (11 ft 6 in) |
Weight | 1590 kg (3500 lb) |
Speed | Mach 1.5 |
Ceiling | 18300 m (60000 ft) |
Range | 480 km (300 miles) |
Propulsion | Pratt & Whitney JT12A-3 turbojet; 12.9 kN (2900 lb) |
Main Sources
[1] Joshua Stoff: "The Thunder Factory", Motorbooks Intl., 1990
[2] Norman J. Bowman: "The Handbook of Rockets and Guided Missiles", Perastadion Press, 1963
[3] Frederick I. Ordway III, Ronald C. Wakeford: "International Missile and Spacecraft Guide", McGraw-Hill, 1960
Back to Directory of U.S. Military Rockets and Missiles, Appendix 4
Last Updated: 5 May 2004