Rocketdyne Engines: F-1 (Rocket Engine), H-1 (Rocket Engine), Hg-3 (Rocket Engine), J-2x, J-2 (Rocket Engine), Pratt & Whitney Rocketdyne,

 
9781156119358: Rocketdyne Engines: F-1 (Rocket Engine), H-1 (Rocket Engine), Hg-3 (Rocket Engine), J-2x, J-2 (Rocket Engine), Pratt & Whitney Rocketdyne,
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Please note that the content of this book primarily consists of articles available from Wikipedia or other free sources online. Pages: 30. Chapters: F-1 (rocket engine), H-1 (rocket engine), HG-3 (rocket engine), J-2X, J-2 (rocket engine), Pratt & Whitney Rocketdyne, RS-18, RS-27A, RS-68, Santa Susana Field Laboratory, Space Shuttle Main Engine. Excerpt: The RS-25, otherwise known as the Space Shuttle Main Engine (SSME), is a liquid-fuel cryogenic rocket engine that was used on NASA's Space Shuttle and is planned to be used on its successor, the Space Launch System. Built in the United States of America by Rocketdyne, the RS-25 burns cryogenic liquid hydrogen & liquid oxygen propellants, with each engine producing 1,859 kN (418,000 lbf) of thrust at liftoff. Although the RS-25 can trace its heritage back to the 1960s, concerted development of the engine began in the 1970s, with the first flight, STS-1, occurring on April 12, 1981. The RS-25 has undergone several upgrades over its operational history to improve the engine's reliability, safety and maintenance load. The engine produces a specific impulse (Isp) of 453 seconds in a vacuum, or 363 seconds at sea level (effective exhaust velocities of 4,440 m/s and 3,560 m/s respectively), consumes 1,340 L (350 US gal) of propellant per second, has a mass of approximately 3.5 tonnes (7,700 pounds) and is capable of throttling between 67% and 111% of its rated power level in one-percent increments. The RS-25 operates at extreme temperatures, with the liquid hydrogen fuel being stored at while the temperature in the combustion chamber reaches , higher than the boiling point of iron. On the Space Shuttle, the RS-25 was used in clusters of three engines mounted in the aft structure of the Orbiter, with fuel being drawn from the external tank. The engines were used for propulsion during the entirety of the spacecraft's ascent, with additional thrust being provided by two solid rocket boosters and the orbiter's two AJ-10-190 Orbital Maneuvering System engines. Following each flight, the engines were removed from the orbiter, inspected and refurbished before being reused on another mission. On the Space Launch System (SLS), expendable versions of the engines are planned to be used in clusters of three, four or five, and draw their propellant from the rocket's core stage. They pr

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