KARI KSR-3 explained
| KARI KSR-3 |
| Designer: | Korea Aerospace Research Institute |
| Date: | 2002[1] |
| Type: | Liquid |
KSR-3 or KSR-III (Korean Sounding Rocket-3)[2] is a South Korean liquid sounding rocket designed by Korea Aerospace Research Institute.[3] It was launched successfully on November 28, 2002 for scientific surveillance purposes.[4] The first test flight of KSR-III was carried out by the KARI rocketry team from Anheung Proving Ground, reaching an altitude of and flying over .[5]
Spec
- Payload: 150 kg
- Apogee: 42.7 km
- Range: 79 km
- Thrust: 13 t
- Weight: 6.1 t
- Diameter: 0.42 m
- Length: 13.5 m
- Burn time: 53 sec
- Launch: November 28, 2002[6]
See also
References
- Book: Eligar Sadeh. The Politics of Space: A Survey. November 2010. Routledge. 978-1-136-88425-2. 80–.
- Book: Si-Chee Tsay. Tatsuya Yokota. Myoung-Hwan Ahn. Society of Photo-optical Instrumentation Engineers, United States. National Aeronautics and Space Administration. Passive optical remote sensing of the atmosphere and clouds IV: 9-10 November, 2004, Honolulu, Hawaii, USA. 2004. SPIE. 9780819456137 .
- Book: C. T. Sun. Proceedings of the American Society for Composites, Seventeenth Technical Conference. 24 October 2002. CRC Press. 978-0-8493-1501-5. 68–.
- Book: Korea Trade & Investment. 2003. Korea Trade Promotion Corporation.
- Book: Brian Harvey. Henk H. F. Smid. Theo Pirard. Emerging Space Powers: The New Space Programs of Asia, the Middle East and South-America. 30 January 2011. Springer Science & Business Media. 978-1-4419-0874-2. 512–.
- Book: Ann Darrin. Beth L. O'Leary. Handbook of Space Engineering, Archaeology, and Heritage. 26 June 2009. CRC Press. 978-1-4200-8432-0. 975–.
Further reading
