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The Convair XFY-1 Pogo is an experimental V/STOL (vertical/short takeoff and landing) aircraft developed during the early years of the Cold War. [1] It was intended to be a high-performance fighter aircraft capable of operating from small warships.
The 3rd Test and Evaluation Squadron (3 TES) (formerly 3rd Space Experimentation Squadron (3 SES)) is a space test and evaluation unit located at Schriever Space Force Base in Colorado. As part of the United States Air Force , the squadron was described, in 2008, as "AFSPC's premier organization for space-based demonstrations, pathfinders and ...
[3] [4] [5] DEL 12 was originally activated as the USAF’s 6565th Test Wing in October 1960 at Vandenberg AFB, CA. The wing was re-designated as the 6565th Test Wing (Development) in December 1960 and was subsequently re-designated, this time as the 6595th Aerospace Test Wing, in April 1961. The wing was inactivated in October 1979.
The Lippisch P.12, P.13a and P.13b were related design projects for a ramjet-powered delta wing interceptor aircraft studied in 1944 by German designer Alexander Lippisch. The P.12 and P.13a were unarmed, relying on reinforced wings to ram its opponent. The P.13a and b were to be powered by producer gas made in-flight from powdered coal.
Ogival delta wing fitted to a Fairey Delta 2 to test the Concorde design. ... Chengdu J-20: China: Supersonic: Fighter: 2011: ... Mach 3+ Lockheed YF-12: US ...
The Convair XF-92 (re-designated from XP-92 in 1948) is an American, delta wing, first-generation jet prototype. Originally conceived as a point-defence interceptor, the design was later used purely for experimental purposes and only one was built.
Data from "C-123 Provider in action" General characteristics Crew: 3 Length: 77 ft 1 in (23.50 m) Wingspan: 110 ft 0 in (33.53 m) Height: 33 ft 10 in (10.31 m) Wing area: 1,222.78 sq ft (113.600 m 2) Airfoil: NACA 23017 Max takeoff weight: 70,000 lb (31,751 kg) limited by tow aircraft to 40,000 pounds (18,000 kg) See also Aviation portal Related development Chase XC-123A Fairchild C-123 ...
Data from DM1 bis DM4 General characteristics Crew: 1 Length: 6.32 m (20 ft 9 in) Wingspan: 6 m (19 ft 8 in) Height: 3.25 m (10 ft 8 in) Wing area: 19 m 2 (200 sq ft) ca Empty weight: 375 kg (827 lb) Gross weight: 460 kg (1,014 lb) Performance Maximum speed: 558 km/h (347 mph, 301 kn) Max speed in terminal velocity dive Stall speed: 72 km/h (45 mph, 39 kn) Maximum glide ratio: 7 See also ...