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Diamant (rocket)

Spacecraft and Launch Vehicles

The Diamant was the first exclusively French expendable launch system and the first satellite launcher not built by the United States or the Soviet Union. Development began in 1962 as the first spacecraft project of the French space agency CNES, drawing on the military Pierres précieuses programme of test rockets. Diamant A made its maiden flight on 26 November 1965 and put the first French satellite, Astérix, into orbit. Three successive versions, A, B and BP4, each had three stages and carried roughly 150 kilograms to a 200 kilometre orbit; fully assembled they weighed 18.4, 26.9 and 20.3 tonnes. Of 12 launch attempts between 1965 and 1975, nine succeeded, the later ones from Kourou in French Guiana. France ended the programme in favour of the European Ariane launcher, which made the national rocket redundant.

Facts
Year
1965 1
Engine Class
Rocket 1
Status
Retired from service 1
Maximum Mass (kg)
18,400 1
Maximum Mass (kg)
20,300 1
Maximum Mass (kg)
26,900 1
Engine
LRBA Valois N2O4/UDMH engine (Diamant B first stage) 1
Engine
Vexin B nitric acid/turpentine engine (Diamant A first stage) 1
Comparison
Body Style
Launch vehicle 1
Connections

Exemplifies

Space Transport, Modes
Source Diamant (rocket) (Wikipedia)

Of Make

Source Aérospatiale (Wikipedia)
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Same As

Also in Space and Astronomy Atlas: the same subject.

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Encyclopedia Astronautica: DiamantDiamant A, development
Quote, Diamant A, development
with SEREB as the prime contractor

Originated In

Also in Geography Atlas: where this subject originated.

Source Diamant (rocket) (Wikipedia)Lead, nationality of the launcher
Quote, Lead, nationality of the launcher
the first exclusively French expendable launch system
Sources
1. Diamant (rocket) (Wikipedia)
  • Lead, maiden flight
    On 26 November 1965, the Diamant A performed its maiden flight.
  • Lead, kind of rocket
    the first exclusively French expendable launch system
  • Variants, Diamant A first stage
    The first stage had a Vexin B nitric acid/turpentine engine supplying a thrust of 274 kN for 93 seconds.
  • Variants, Diamant B first stage
    Its LRBA Valois N2O4/UDMH engine developed a thrust of 315 kN for 116 seconds.
  • Variants, Diamant A mass
    Completely assembled, a Diamant A was 18.95 metres high and weighed 18.4 metric tons.
  • Variants, Diamant B mass
    Completely assembled, a Diamant B was 23.5 metres high and weighed 26.9 metric tons.
  • Variants, Diamant BP4 mass
    Completely assembled, a Diamant BP4 measured 22.68 metres high and weighed 20.3 metric tons.
  • Development, end of the programme
    France ultimately decided to discontinue further launches using Diamant in favour of the newer Ariane platform.
  • Lead, nationality of the launcher
    the first exclusively French expendable launch system
View the Source
Aérospatiale (Wikipedia)
Of Make: Aérospatiale, Products, space-related products
Quote, Of Make: Aérospatiale, Products, space-related products
Diamant (rocket)
View the Source
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