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Hammaguira Brigitte
Part of Hammaguira
VE, SSBS, MSBS, Diamant launch complex. Brigitte, CIEES B2
First Launch: 1962-12-19. Last Launch: 1967-02-15. Number: 44 . Longitude: -3.04 deg. Latitude: 30.89 deg.
Country:
Algeria.
Spacecraft:
Asterix,
D,
Diadem.
Launch Vehicles:
Agate,
VE10A Aigle,
Emeraude VE121,
Saphir VE231,
SSBS S112,
Diamant A,
MSBS M112.
Launch Sites:
Hammaguira.
1963 March 5 - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
Stromboli.
Launch Vehicle:
VE10A Aigle.
- Test mission - .
Nation: France.
Agency: ONERA.
Apogee: 20 km (12 mi).
1963 May 18 - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
Launch Vehicle:
Agate.
- Test mission - .
Nation: France.
Agency: ONERA.
Apogee: 20 km (12 mi).
1963 May 21 - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
Launch Vehicle:
Agate.
- Test mission - .
Nation: France.
Agency: ONERA.
Apogee: 20 km (12 mi).
1964 June 15 - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
Diamant.
Launch Vehicle:
Emeraude VE121.
FAILURE: Failure.
- Test mission - .
Nation: France.
Agency: CNES.
Apogee: 0 km (0 mi).
1964 June 17 - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
Diamant.
Launch Vehicle:
Emeraude VE121.
FAILURE: Failure.
- Test mission - .
Nation: France.
Agency: CNES.
Apogee: 0 km (0 mi).
1964 October 20 - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
Diamant.
Launch Vehicle:
Emeraude VE121.
FAILURE: Failure.
- Test mission - .
Nation: France.
Agency: CNES.
Apogee: 0 km (0 mi).
1964 November 2 - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
Stromboli.
Launch Vehicle:
VE10A Aigle.
- Test mission - .
Nation: France.
Agency: ONERA.
Apogee: 20 km (12 mi).
1965 February 27 - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
Diamant.
Launch Vehicle:
Emeraude VE121.
- Test mission - .
Nation: France.
Agency: CNES.
Apogee: 200 km (120 mi).
1965 May 13 - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
Diamant.
Launch Vehicle:
Emeraude VE121.
- Test mission - .
Nation: France.
Agency: CNES.
Apogee: 200 km (120 mi).
1965 July 5 - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
Diamant.
Launch Vehicle:
Saphir VE231.
- Re-entry Vehicle test - .
Nation: France.
Agency: ONERA.
Apogee: 1,000 km (600 mi).
1965 July 10 - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
Diamant.
Launch Vehicle:
Saphir VE231.
FAILURE: Failure.
- Re-entry Vehicle test - .
Nation: France.
Agency: ONERA.
Apogee: 50 km (31 mi).
1965 October 9 - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
Diamant.
Launch Vehicle:
Saphir VE231.
- Re-entry Vehicle test - .
Nation: France.
Agency: ONERA.
Apogee: 1,150 km (710 mi).
1965 October 23 - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
MSBS.
Launch Vehicle:
SSBS S112.
- Essai 1 test - .
Nation: France.
Agency: DMA.
Apogee: 50 km (31 mi).
1965 November 3 - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
MSBS.
Launch Vehicle:
SSBS S112.
- Essai 2 test - .
Nation: France.
Agency: DMA.
Apogee: 50 km (31 mi).
1965 November 26 - .
14:47 GMT - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
Diamant.
Launch Vehicle:
Diamant A.
- Asterix 1 - .
Payload: A 1. Mass: 42 kg (92 lb). Nation: France.
Agency: CNES.
Class: Technology.
Type: Navigation technology satellite. Spacecraft: Asterix.
USAF Sat Cat: 1778 . COSPAR: 1965-096A. Apogee: 1,697 km (1,054 mi). Perigee: 527 km (327 mi). Inclination: 34.30 deg. Period: 107.50 min. First French satellite. French scientific satellite 'A-I'. Launched from Hammaguir (Algeria) in rder to test the 'Diamant' launching vehicle for the first time..
1966 February 17 - .
08:33 GMT - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
Diamant.
Launch Vehicle:
Diamant A.
- Diapason - .
Payload: D-1A. Mass: 19 kg (41 lb). Nation: France.
Agency: CNES.
Class: Earth.
Type: Geodetic satellite. Spacecraft: D.
USAF Sat Cat: 2016 . COSPAR: 1966-013A. Apogee: 2,484 km (1,543 mi). Perigee: 502 km (311 mi). Inclination: 34.10 deg. Period: 115.80 min. Scientific satellite 'D-I' launched from Hammaguir (Algeria)..
1966 March 13 - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
Diamant.
Launch Vehicle:
Saphir VE231.
- Re-entry Vehicle test - .
Nation: France.
Agency: ONERA.
Apogee: 1,000 km (600 mi).
1966 March 18 - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
Diamant.
Launch Vehicle:
Saphir VE231.
- Re-entry Vehicle test - .
Nation: France.
Agency: CNES.
Apogee: 1,000 km (600 mi).
1966 March 28 - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
Diamant.
Launch Vehicle:
Saphir VE231.
- Re-entry Vehicle test - .
Nation: France.
Agency: ONERA.
Apogee: 1,000 km (600 mi).
1966 April 5 - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
Diamant.
Launch Vehicle:
Saphir VE231.
- Re-entry Vehicle test - .
Nation: France.
Agency: ONERA.
Apogee: 1,000 km (600 mi).
1966 May 26 - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
MSBS.
Launch Vehicle:
MSBS M112.
- Essai 1 test - .
Nation: France.
Agency: DMA.
Apogee: 50 km (31 mi).
1966 June 1 - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
MSBS.
Launch Vehicle:
MSBS M112.
- Essai 2 test - .
Nation: France.
Agency: DMA.
Apogee: 50 km (31 mi).
1966 June 23 - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
Diamant.
Launch Vehicle:
Saphir VE231.
- Re-entry Vehicle test - .
Nation: France.
Agency: ONERA.
Apogee: 1,000 km (600 mi).
1966 October 5 - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
Diamant.
Launch Vehicle:
Saphir VE231.
- Re-entry Vehicle test - .
Nation: France.
Agency: ONERA.
Apogee: 1,000 km (600 mi).
1966 October 28 - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
Diamant.
Launch Vehicle:
Saphir VE231.
- Re-entry Vehicle test - .
Nation: France.
Agency: ONERA.
Apogee: 1,000 km (600 mi).
1966 November 2 - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
Diamant.
Launch Vehicle:
Saphir VE231.
- Re-entry Vehicle test - .
Nation: France.
Agency: ONERA.
Apogee: 1,000 km (600 mi).
1966 December 2 - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
Diamant.
Launch Vehicle:
Saphir VE231.
FAILURE: Failure.
- Re-entry Vehicle test - .
Nation: France.
Agency: ONERA.
Apogee: 50 km (31 mi).
1966 December 13 - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
Diamant.
Launch Vehicle:
Saphir VE231.
- Re-entry Vehicle test - .
Nation: France.
Agency: ONERA.
Apogee: 1,000 km (600 mi).
1967 January 19 - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
Diamant.
Launch Vehicle:
Saphir VE231.
- Re-entry Vehicle test - .
Nation: France.
Agency: ONERA.
Apogee: 1,000 km (600 mi).
1967 January 27 - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
Diamant.
Launch Vehicle:
Saphir VE231.
- Re-entry Vehicle test - .
Nation: France.
Agency: ONERA.
Apogee: 1,000 km (600 mi).
1967 February 8 - .
09:39 GMT - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
Diamant.
Launch Vehicle:
Diamant A.
FAILURE: Partial Failure - injected into too low an orbit..
Failed Stage: 3.
- Diademe 1 - .
Payload: Diademe D-1C. Mass: 23 kg (50 lb). Nation: France.
Agency: CNES.
Class: Earth.
Type: Geodetic satellite. Spacecraft: Diadem.
USAF Sat Cat: 2674 . COSPAR: 1967-011A. Apogee: 1,084 km (673 mi). Perigee: 545 km (338 mi). Inclination: 40.00 deg. Period: 101.20 min. Orbit too low. Launch time of Diadem I was 10:39:40 on 8 Feb 1967. Launch time of Diadem II was 11:06:57 on 15 Feb 1967..
1967 February 15 - .
10:06 GMT - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
Diamant.
Launch Vehicle:
Diamant A.
- Diademe 2 - .
Payload: Diademe D-1D. Mass: 23 kg (50 lb). Nation: France.
Agency: CNES.
Class: Earth.
Type: Geodetic satellite. Spacecraft: Diadem.
USAF Sat Cat: 2680 . COSPAR: 1967-014A. Apogee: 1,733 km (1,076 mi). Perigee: 584 km (362 mi). Inclination: 39.40 deg. Period: 108.50 min. Launch time of Diadem I was 10:39:40 on 8 Feb 1967. Launch time of Diadem II was 11:06:57 on 15 Feb 1967. .
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