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The Triumph Rocket III is a three-cylinder motorcycle made by Triumph Motorcycles Ltd. At 2,294 cc (140.0 cu in) it had the largest- displacement engine of any production motorcycle [ 4 ] until 2019 when Triumph released the Triumph Rocket 3 .
The Triumph Rocket 3 is a motorcycle by manufacturer Triumph Motorcycles Ltd. [2] Like its predecessor, the Rocket III , it is characterized by an engine that, at 2,458 cc (150.0 cu in), is much larger than any other production motorcycle and consequently has much higher torque. [ 3 ]
The Triumph Trident and BSA Rocket 3 was a technically advanced, high-performance roadster (or standard) motorcycle made by Triumph Engineering and BSA (both companies part of the Birmingham Small Arms Company) from 1968 to 1975, and sold under both the Triumph and BSA marques. [1]
Rocket 3 may refer to: Triumph Rocket III, a motorcycle by Triumph Motorcycles Ltd; Triumph Rocket 3, the successor of Triumph Rocket III; BSA Rocket 3/Triumph ...
Rocket 4 is to be a new launch vehicle, much larger than the previous Rocket 3.3 and capable of carrying up to 600 kg (1,300 lb) to orbit, and 350 kg (770 lb) to a sun-synchronous orbit. [ 17 ] [ 18 ] The vehicle's upper stage is designed to integrate the Ursa Major Hadley engine, [ 19 ] while the booster will feature 2 70,000 lbf (310 kN ...
The rocket was used as part of a project for the DARPA Launch Challenge, although challenge's deadline passed before any Rocket 3 launches. Launches of Rocket 3.0 and 3.1 resulted in failure, while Astra claimed success after Rocket 3.2 failed to reach orbit. Rocket 3.3 was larger than previous Rocket 3 variants, and multiple vehicles were ...
Rocket 3, Rocket 4 Rocket 3 retired in August 2022 [40] Firefly Aerospace: Firefly Alpha, Firefly MLV IHI Corporation: Epsilon Some R&D by JAXA Mitsubishi Heavy Industries: H-IIA R&D done by JAXA. [226] Northrop Grumman Innovation Systems: Antares, Minotaur Own launchers, funded by NASA Rocket Lab: Neutron, Electron SpaceX: Falcon 9, Falcon ...
Engine Origin Designer Vehicle Status Use Propellant Power cycle Specific impulse (s) [a] Thrust (N) [a] Chamber pressure (bar) Mass (kg) Thrust: weight ratio [b] Oxidiser: fuel ratio