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The FJ33 has a dry weight of less than 300 lb (140 kg), overall diameter of 18.36 in (466 mm), 38.43 in (976 mm) overall length, and produces between 1,000 lbf (4,400 N) and 1,800 lbf (8,000 N) static thrust.
Thrust2 is a British jet car, which held the world land speed record from 4 October 1983 to 25 September 1997. [a]The Thrust2 is powered by a single Rolls-Royce Avon jet engine sourced from an English Electric Lightning, and has a configuration somewhat resembling that of the mid-1960s-era J79 turbojet-powered land speed record cars of Art Arfons, collectively known as the "Green Monster" cars.
After the Advanced Technology Fan Integrator demonstrator first ran on March 17, 2001, which became the PW1000G, Pratt & Whitney Canada was searching for a launch customer for the initially geared PW800, in the 10,000–19,000 lbf (44–85 kN) thrust range, bridging the gap between P&WC's PW300 and P&W's PW6000, intended for the regional- and ...
A proposed 9,000 lbf (40 kN; 4,100 kgf) thrust version with a new high-pressure turbine ceramic-matrix composite tailcone [15] GMA 3010 / AE 3010 A 10,000 lbf (44.5 kN; 4,540 kgf) thrust variant, which was to power the Yakovlev Yak-77 twin-engine business jet [ 16 ] as a derated variant of the GMA 3012 with a 44 in diameter (112 cm) fan [ 17 ]
Data from Cliche and Kitplanes General characteristics Crew: one Length: 15 ft 6 in (4.72 m) Wingspan: 22 ft 0 in (6.71 m) Height: 5 ft 4 in (1.63 m) Wing area: 140 sq ft (13 m 2) Empty weight: 247 lb (112 kg) Gross weight: 500 lb (227 kg) Fuel capacity: 5 US gallons (19 litres) Powerplant: 1 × Rotax 277 single cylinder two stroke piston aircraft engine, 28 hp (21 kW) Performance Maximum ...
This variant is an uprated model of the 60-1 engines, with thrust increased to 3.7 kN (830 lbf). [2] TRI 60-2 071: This model powers the Aerospatiale C.22 target drone, and is slight uprated to 4.0 kN (900 lbf). TRI 60-2 074: This model powers several versions of the MQM-107 Streaker drone. TRI 60-2 077: This model powers the RBS-15 anti-ship ...
(PW1212) 12,000 lbf (53 kN) thrust version of the J52-P-408 with an improved low pressure turbine (LPT) and faster acceleration. Designed for the EA-6B and was additionally marketed as an upgrade for the A-4. The J52-P-409 was also proposed as a cost-effective upgrade to the A-6E as an alternative to the A-6F Intruder II, [9] but was not purchased.
Specifications called for a supersonic V/STOL strike fighter with a combat radius of 460 kilometres (250 nmi), a cruise speed of Mach 0.92, and a dash speed of Mach 1.5. [8] During the early 1960s, Hawker commenced work upon developing a supersonic version of the P.1127, designated the P.1150 , culminating in the abortive Hawker P.1154 .