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Diamant A - Diamant A - COSPAR 1965-096 28,983 bytes. 153 x 474 pixels. |
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Family: Ariane. Country: France. Status: Hardware.
First French indigenous satellite launch vehicle.
SpecificationsLaunches: 4. Failures: 1. Success Rate: 75.00% pct. First Launch Date: 26 November 1965. Last Launch Date: 15 February 1967. LEO Payload: 160 kg. to: 200 km Orbit. Liftoff Thrust: 27,070 kgf. Total Mass: 18,400 kg. Core Diameter: 1.3 m. Total Length: 20.0 m. Flyaway Unit Cost $: 5.70 million. in 1985 unit dollars.
- Stage Number: 1. 1 x Diamant-1 Gross Mass: 14,685 kg. Empty Mass: 1,946 kg. Thrust (vac): 30,750 kgf. Isp: 251 sec. Burn time: 100 sec. Isp(sl): 221 sec. Diameter: 1.3 m. Span: 2.3 m. Length: 9.8 m. Propellants: N2O4/UDMH No Engines: 4. Vexin B
- Stage Number: 2. 1 x Diamant-2 Gross Mass: 2,815 kg. Empty Mass: 540 kg. Thrust (vac): 12,245 kgf. Isp: 255 sec. Burn time: 39 sec. Isp(sl): 225 sec. Diameter: 0.8 m. Span: 0.8 m. Length: 4.6 m. Propellants: N2O4/UDMH No Engines: 1. Topaze
- Stage Number: 3. 1 x Diamant-3 Gross Mass: 703 kg. Empty Mass: 68 kg. Thrust (vac): 3,000 kgf. Isp: 211 sec. Burn time: 39 sec. Isp(sl): 211 sec. Diameter: 0.7 m. Span: 0.7 m. Length: 2.0 m. Propellants: Solid No Engines: 1. P6
Diamant Chronology
1965 Nov 26 - - 14:47 GMT. LV Configuration: Diamant A s/n No. 1. Launch Site: Hammaguira . Launch Complex: Brigitte.
1966 Feb 17 - - 08:33 GMT. LV Configuration: Diamant A s/n No. 2. Launch Site: Hammaguira . Launch Complex: Brigitte.
1967 Feb 8 - - 09:39 GMT. LV Configuration: Diamant A s/n No. 3. Launch Site: Hammaguira . Launch Complex: Brigitte. FAILURE: Partial Failure.
1967 Feb 15 - - 10:06 GMT. LV Configuration: Diamant A s/n No. 4. Launch Site: Hammaguira . Launch Complex: Brigitte.
Bibliography:- 34 - Gatland, Kenneth, Missiles and Rockets, Macmillan, New York, 1975.
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Last update 12 March 2001.
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