Castor A
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] Experiencing one failed launch, it had a success rate of approximately 83.3%.[1][3]
Launches
[edit]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
[edit]Images
[edit]- First Castor (CRX-01) at CELPA Chamical
- Castor launch preparations
References
[edit]- 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 "Castor (A)". www.astronautix.com. Retrieved 2023-10-20.
- 1 2 3 4 5 6 "NTI: Country Overviews: Argentina: Missile Chronology". 2006-02-19. Archived from the original on 2006-02-19. Retrieved 2023-07-27.
{{cite web}}: CS1 maint: bot: original URL status unknown (link) - 1 2 3 4 5 6 7 8 9 10 "Castor". Gunter's Space Page. Retrieved 2023-07-27.