Engineering:Castor A
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The Castor A was an Argentine sounding rocket designed in 1969 by the Instituto de Investigaciones Aeronáuticas y Espaciales (IIAE).[1][2]
The rocket featured a two-stage configuration, utilizing five Canopus II rockets (four in the first stage and one in the second).[1][2] It was capable of placing a 75 kg (165 lb) payload at a 400 km altitude.[1]
Throughout its operational lifespan, the Castor A was launched seven times.[1][3] It experienced one failure during one of its launches, thus achieving a success rate of approximately 83.3%.[1][3]
Launches
Castor was launched seven times:[1][3]
Date | Mission Type | Nation | Agency | Apogee | Launch Site |
---|---|---|---|---|---|
December 22, 1969 | Test mission | Argentina | IIAE | 52 km | CELPA Chamical[1][3] |
December 19, 1970 | Test mission | Argentina | IIAE | 45 km | CELPA Chamical[1][3] |
November 22, 1973 | Ion beam Ionosphere mission | Germany | MPE | 406 km | CELPA Chamical[1][3] |
September 30, 1975 | Ionosphere mission | Germany | MPE | 400 km | Vice Commodore Marambio Base, Antarctica[1][3] |
October 3, 1975 | Ionosphere mission | Germany | MPE | 400 km | Vice Commodore Marambio Base, Antarctica[1][3] |
March 21, 1979, 11:49 PM | Spread F Barium release mission | Germany | DFVLR | Failure | Chilca, Peru[1][3] |
March 22, 1979, 11:59 PM | Spread F Barium release mission | Germany | DFVLR | 268 km | Chilca, Peru[1][3] |
Specifications
Images
References
- ↑ 1.00 1.01 1.02 1.03 1.04 1.05 1.06 1.07 1.08 1.09 1.10 1.11 1.12 1.13 1.14 1.15 1.16 "Castor (A)". http://www.astronautix.com/c/castora.html.
- ↑ 2.0 2.1 2.2 2.3 2.4 2.5 "NTI: Country Overviews: Argentina: Missile Chronology". 2006-02-19. http://www.nti.org/e_research/profiles/Argentina/Missile/1734.html.
- ↑ 3.0 3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 "Castor" (in en). https://space.skyrocket.de/doc_lau/castor_arg.htm.
Original source: https://en.wikipedia.org/wiki/Castor A.
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