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Hammaguira Brigitte
Part of Hammaguira Family
VE, SSBS, MSBS, Diamant launch complex. Brigitte, CIEES B2

First Launch: 1962-12-19. Last Launch: 1967-02-15. Number: 44 . Longitude: -3.0357 deg. Latitude: 30.8935 deg.



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: 34.3000 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: 34.1000 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: 40.0000 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: 39.4000 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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