Engineering:Rocketdyne XRS-2200
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Short description: Aerospike rocket engine by Rocketdyne
 Rocketdyne XRS-2200 hotfire test | |
| Country of origin | United States |
|---|---|
| Date | 1999 |
| Designer | Rocketdyne |
| Manufacturer | Rocketdyne |
| Application | X-33 |
| Predecessor | J-2 |
| Status | Experimental |
| Liquid-fuel engine | |
| Propellant | LOX / LH2 |
| Cycle | Gas Generator |
| Configuration | |
| Nozzle ratio | 58:1 |
| Performance | |
| Thrust (vac.) | 1,184 kN (266,000 lbf) |
| Thrust (SL) | 909 kN (204,000 lbf) |
| Chamber pressure | 58 bar (840 psi) |
| Isp (vac.) | 439 seconds (4.31 km/s) |
| Isp (SL) | 339 seconds (3.32 km/s) |
| Dimensions | |
| Length | 2.01 m (6 ft 7 in) |
The Rocketdyne XRS-2200 was an experimental linear aerospike engine developed in the mid-1990s for the Lockheed Martin X-33 program.[1][2][3] The XRS-2200 engine's powerpack (Turbomachinery and Gas Generator) was derived from the Rocketdyne J-2 engine, the upper stage engine of the Saturn V moon rocket developed under the Apollo Program in the 1960's. The XRS-2200 used the J-2's combustion cycle and propellant choice.[4]
Rocketdyne intended to develop the subscale XRS-2200 into the RS-2200 for use on the VentureStar. While the X-33 program was cancelled, two XRS-2200 engines were produced and tested.[5]
References
- ↑ "Boeing Rocketdyne XRS-2200 Linear Aerospike". https://engineering.purdue.edu/~propulsi/propulsion/rockets/liquids/xrs2200.html.
- ↑ "XRS-2200 Link". Washington D.C., U.S.: NASA Headquarters. https://www.hq.nasa.gov/office/pao/History/x-33/xrs2200.htm.
- ↑ Rowbotham, Maureen (1999). "XRS-2200 linear aerospike engine - Use of Pro/ENGINEER for determining mass properties". 35th Joint Propulsion Conference and Exhibit. U.S.: American Institute of Aeronautics and Astronautics. doi:10.2514/6.1999-2334. https://arc.aiaa.org/doi/abs/10.2514/6.1999-2334. Retrieved 2019-09-29.
- ↑ "XRS-2200". Encyclopedia Astronautica. http://www.astronautix.com/x/xrs-2200.html.
- ↑ D'Agostino, M.G. (January 2001). "X-33 XRS-2200 Linear Aerospike Engine Sea Level Plume Radiation". NASA Technical Reports Server. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20020017580.pdf.
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