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Diameter. 1.56 m (5.1 ft) Dry mass. 435 kg. Used in. Upper stage of GSLV Mk.II. The CE-7.5 is a cryogenic rocket engine developed by the Indian Space Research Organisation to power the upper stage of its GSLV Mk-2 launch vehicle. The engine was developed as a part of the Cryogenic Upper Stage Project (CUSP).
The smallest-displacement engine of the 385 engine family, the 370 was introduced in 1977, replacing the 361 cu in (5.9 L) 360 Truck (FT) V8. Sharing its 3.59-inch stroke with the 429, the 370 was designed with a downsized 4.05-inch bore (shared with its predecessor and the 390 V8).
The F-1 is a rocket engine developed by Rocketdyne. The engine uses a gas-generator cycle developed in the United States in the late 1950s and was used in the Saturn V rocket in the 1960s and early 1970s. Five F-1 engines were used in the S-IC first stage of each Saturn V, which served as the main launch vehicle of the Apollo program.
Rutherford is a liquid-propellant rocket engine designed by aerospace company Rocket Lab [ 8] and manufactured in Long Beach, California. [ 9] The engine is used on the company's own rocket, Electron. It uses LOX (liquid oxygen) and RP-1 (refined kerosene) as its propellants and is the first flight-ready engine to use the electric-pump-fed cycle.
Its Rutherford engines are the first electric-pump-fed engine to power an orbital-class rocket. [17] Electron is often flown with a kickstage or Rocket Lab's Photon spacecraft. Although the rocket was designed to be expendable , Rocket Lab has recovered the first stage twice and is working towards the capability of reusing the booster. [ 18 ]
The 4M50 is a series of 4-cylinder diesel engines with 4899 cc, bore × stroke 114 × 120mm, gear driven, DOHC 4 valves per cylinder, and common rail direct injection with turbocharging and intercooler. [ 6] 4M50-T3 – 103 kW, 412 Nm. 02/2004- Mitsubishi Fuso Canter. 4M50-4AT4 – 110 kW at 2700 rpm, 441 Nm at 1600 rpm.
A liquid-propellant rocket or liquid rocket utilizes a rocket engine burning liquid propellants. (Alternate approaches use gaseous or solid propellants .) Liquids are desirable propellants because they have reasonably high density and their combustion products have high specific impulse ( Isp). This allows the volume of the propellant tanks to ...
The Gen IV LS9 is a supercharged 6,162 cc (6.2 L; 376.0 cu in) engine, based on the LS3; the LS7 block was not used because of the higher cylinder pressures created by the supercharger requiring the thicker cylinder walls of the LS3. It has a bore and stroke of 103.25 mm × 92 mm (4.065 in × 3.622 in).
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