NEXT SPACEFLIGHT

Status

Partial Failure

Diadème 1

Launch Time
Wed Feb 08, 1967 09:39 UTC

The thrust of the third stage was lower than expected, and the orbit reached was also lower than expected. However, the satellite was able to fulfill its mission.

Rocket

Diamant A
Image Credit: CNES
Armée de l'Air
Status: Retired
Liftoff Thrust: 274 kN
Payload to LEO: 80 kg
Payload to GTO: 0 kg
Stages: 3
Strap-ons: 0
Rocket Height: 18.49 m
Fairing Diameter: 0.65 m
Fairing Height: 2.16 m

Mission Details

Diadème 1

The French satellites Diadème 1 and Diadème 2 were geodetic missions.

These satellites are magnetically stabilized which limits their trackability in the southern hemisphere. Diadème has the following instrumentation onboard:

- Dual frequency Doppler transmitters
- Retroreflector array consisting of 2 flattened truncated cones with 77 cube corners per cone for a total of 144 cube corners.

Payloads: 1
Total Mass: 23.0 kg
Low Earth Orbit

Location

Brigitte, Hammaguir, Algeria, France

Stats

1967

12th orbital launch attempt

Armée de l'Air

3rd mission
1st mission of 1967

Diamant

3rd mission
1st mission of 1967