Vesta (rocket)
 Vesta 1 | |
| Country of origin | France |
|---|---|
| Size | |
| Height | 10.2 m |
| Diameter | 1 m |
| Mass | 5.1 tons |
| Stages | 1 |
| Capacity | |
| Launch history | |
| Launch sites | CIEES, Guiana Space Centre |
| First stage | |
| Thrust | 160 kN |
The Vesta sounding rocket, conceived in 1962 by the Laboratoire de recherches balistiques et aérodynamiques (LRBA), a specialized French Army research facility focused on liquid-propelled rocket development.[1][2][3] The initial letter "V" in its name is derived from the city of Vernon.
It was the outcome of an initiative by CNES with the purpose of enabling transportation of more substantial experiments to greater altitudes than the Véronique sounding rocket, also created by the LRBA and in active service at the time.[1][2]
Technical details
Operated by a 160 kN thrust engine using a combination of nitric acid and turpentine as propellants, the Vesta rocket was 10.2 meters tall with a diameter of 1 meter.[3][4] Weighing 5.1 tons excluding its payload, Vesta had the capability to send a 500 kg to an altitude of 400 km.[1][2][3]
Launches
Between 1965 and 1969 a total of five Vesta rockets were launched.[5] These launches took place from both CIEES and Kourou.[1][2][3][5] The first two launches primarily served as validation tests for the rocket's operation,[1] whereas the subsequent three carried out scientific experiments.[2][3]
A pig-tailed macaque named Martine was launched on March 7, 1967, and another named Pierette on March 13.[2] These suborbital flights reached 243 km (151 mi) and 234 km (145 mi), respectively. Martine became the first monkey to survive more than a couple of hours after flying above the international definition of the edge of space. (Ham and Enos, launched earlier by the United States, were chimpanzees).[6]
| Date | Site | Vehicle | Mission | Apogee | Results |
|---|---|---|---|---|---|
| 15 October 1965 | CIEES | Vesta 01 | FU123 Technology | 187 km | Success |
| 25 October 1965 | CIEES | Vesta 03 | FU123 Technology | 109 km | Partial success |
| 7 March 1967 | CIEES | Vesta 04 | FU147 Biology | 243 km | Success |
| 13 March 1967 | CIEES | Vesta 05 | FU147 Biology | 234 km | Success |
| 8 November 1969 | Kourou | Vesta 02 | FU189 Astronomy | 204 km | Partial success |
See also
References
- ^ a b c d e f Serra, Jean-Jacques (2008-06-14). "Veronique and Vesta". Rockets in Europe. Archived from the original on 2007-10-20. Retrieved 2023-08-26.
- ^ a b c d e f g Capdevila, Didier. "CHRONOLOGIE ARIANE » VERONIQUE ET VESTA". Capcom Espace. Retrieved 2023-08-26.
- ^ a b c d e f "Vesta". astronautix.com. Retrieved 2023-08-26.
- ^ "Vesta-1". astronautix.com. Retrieved 2023-08-26.
- ^ a b c Gunter D., Krebs. "Vesta". Gunter's Space Page. Retrieved 2023-08-26.
- ^ Burgess & Dubbs (2007), p. 387.