Bérénice (rocket)
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Bérénice was the designation of a four-stage French atmospheric reentry test rocket, developed by O.N.E.R.A. (Office National d'Etudes et de Recherches Aérospatiales).[1][2][3][4][5]
Description
Bérénice was Script error: No such module "convert". long, possessed a diameter of Script error: No such module "convert". and weighed Script error: No such module "convert". at launch. The takeoff thrust of Bérénice, which could carry a payload of Script error: No such module "convert". to a height of Script error: No such module "convert"., amounted to Script error: No such module "convert".. The first stage, a SEPR-739 Stromboli, was stabilised by four SEPR-P167 rockets developing Script error: No such module "convert"..[1][4][5] The second stage consisted of a SEPR-740 Stromboli, almost identical to the first stage.[1][4][5] The third stage was a SEPR-P200 Tramontane and the fourth stage comprised a Mélanie rocket and payload.[2][3][4][5]
Launches
The twelve production rockets, Bérénice 001 to Bérénice 012, were launched by ONERA from Ile du Levant from 1962 to 1966.[1][3]
| Date | Mission Description | Apogee (km) |
|---|---|---|
| 1962 June 27 | Re-entry Vehicle test | 270 |
| 1962 Q3 | Re-entry Vehicle test | 270 |
| 1962 July 6 | Re-entry Vehicle test | 270 |
| 1962 November 1 | Re-entry Vehicle test | 270 |
| 1963 June 27 | Re-entry Vehicle test | 270 |
| 1963 July 3 | Re-entry Vehicle test | 270 |
| 1964 | Re-entry Vehicle test | 270 |
| 1964 | Re-entry Vehicle test | 270 |
| 1964 October 1 | Re-entry Vehicle test | 250 |
| 1964 October 1 | Re-entry Vehicle test | 250 |
| 1965 | Re-entry Vehicle test | 270 |
| 1966 | Titus test / solar mission | 270 |
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See also
References
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