1.8KS7800
| Country of origin | United States |
|---|---|
| Date | 1957 |
| Designer | Aerojet |
| Status | Retired |
| Solid-fuel motor | |
| Performance | |
| Thrust (vac.) | 35 kN |
| Dimensions | |
| Length | 1.3 m |
| Diameter | 0.2 m |
1.8KS7800 is a solid propellant rocket engine designed by Aerojet and used in the AIM-7A, AIM7B and AIM7C Sparrow missiles.[1] The designation 1.8KS7800 means that the engine burns during 1.8 seconds and generates 7,800 pounds of thrust.[2][3][4]
References
- ↑ Parsch, Andreas (April 7, 2007). "Raytheon AAM-N-2,3,6/AIM-101/AIM-7/RIM-7 Sparrow". Retrieved March 2, 2010.
- ↑ "Rocket Motor, Solid Fuel, 1.KS 7800, Sparrow II Missile". Smithsonian National Air and Space Museum. Retrieved March 2, 2010.
- ↑ Wade, Mark (2008). "1.8KS7800". Retrieved March 2, 2010.
- ↑ McDowell, Jonathan (February 2007). "Stages". Retrieved 2010-03-02.
This article is issued from
Wikipedia.
The text is licensed under Creative Commons - Attribution - Sharealike.
Additional terms may apply for the media files.