Centaure (rocket)
Centaure was a two-stage French sounding rocket consisting of a Venus first stage and a Belier second stage. It belongs to a family of solid-propellant rockets consisting of the Belier, Centaure, Dragon, Dauphin, and Eridan.
Centaur rocket | |
| Country of origin | France |
|---|---|
| Application | high altitude research |
| sounding rocket | |
It was operated by Sud-Aviation between 1961 and 1986. Centaure rockets were launched from the CIEES/Hammaguir missile range, Reggane, CELPA, Salto di Quirra, Esrange, Thumba, Sonmiani, and Andøya.
It had a maximum payload of 60 kg, an apogee of 130-146 km, a launch thrust of 44 kN, a launch weight of 500-600 kg, a diameter of 0.28 m and a length of 5.9-6.3 m.
Wikimedia Commons has media related to Centaure (rocket).
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.