Centaure (rocket)

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Template:Infobox rocket engineCentaure was a two-stage French sounding rocket consisting of a Venus first stage and a Belier second stage.[1][2][3] It belongs to a family of solid-propellant rockets consisting of the Belier, Centaure, Dragon, Dauphin, and Eridan.[2][3]

File:Sudav-belier-family.gif
Sud-Aviation Belier rockets evolution

It was operated by Sud-Aviation between 1961 and 1986.[1][3][4] Centaure rockets were launched from the CIEES/Hammaguir missile range, Reggane, CELPA, Salto di Quirra, Esrange, Thumba, Sonmiani, and Andøya.[3]

It had a maximum payload of 60 kg, an apogee of 130-146 km,[3] 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.

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Versions

There were various versions of Centaure rockets:[2][4][5][6][7][8]

Version Stages Gross mass (kg) Height (m) Diameter (m) Apogee (km)
Centaure Venus + Belier 457 6.02 0.28 140
Centaure 1 Venus + Belier 600 5.9 0.28 130
Centaure 2A Venus + Belier II 600 5.9 0.28 146
Centaure 2B Venus + Belier II 500 6.3 0.28 146
Centaure 2C Venus + Belier II 600 5.9 0.28 146

Launches

A large number of Centaure rockets was launched between 1961 and 1986:[4][5][6][7][8]

See also

References

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External links

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