Reaction Motors XLR99
The Reaction Motors LR99 engine was the first large, throttleable, restartable liquid-propellant rocket engine. Development began in the 1950s by the Reaction Motors Division of Thiokol Chemical Company to power the North American X-15 hypersonic research aircraft. It could deliver up to 57,000 pounds force (254 kN) of thrust with an Isp of 279 seconds (239 seconds sl). Thrust was variable from 50 to 100 percent, and the restart capability allowed it to be shut down and restarted during flight when necessary.
|An XLR-99 rocket engine.|
|Type||Liquid-propellant rocket engine|
|National origin||United States|
|Major applications||North American X-15|
Design and development
After one hour of operation, the XLR99 required an overhaul. Operating times nearly twice that were recorded in tests, but declared largely unsafe. The basic X-15 aircraft carried fuel for about 83 seconds of full-powered flight, while the X-15A-2 carried fuel for just over 150 seconds. Therefore, each XLR99 was capable, in theory, of between 20 and 40 flights before an overhaul.
Like many other liquid-fuel rocket engines, the XLR99s used regenerative cooling, in that the thrust chamber and nozzle had tubing surrounding it, through which the propellant and oxidizer passed before being burned. This kept the engine cool, and preheated the fuel. The basic engine has a mass of 910 lb (410 kg).
The LR-99 was used exclusively to power the X-15 research aircraft after initial trials that used a pair of Reaction Motors XLR11s.
- Type: liquid-fuelled rocket engine
- Length: 82 in (2,083 mm)
- Diameter: 39.3 in (998 mm) at the nozzle
- Dry weight: 910 lb (412.8 kg)
- Fuel: liquid ammonia (LNH3)
- Oxidiser: liquid oxygen (LO2 / LOX)
- Pumps: turbopumps 200 lb/s (90.7 kg/s) driven by High-test peroxide (H2O2) decomposed by a catalyst
- Wilkinson, Paul H. (1964). Aircraft engines of the World 1964/65 (20th ed.). London: Sir Isaac Pitman & Sons Ltd. p. 39.
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