Diamant

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Diamant
Diamant P6230215.JPG
Function Small launch vehicle
Manufacturer SEREB
Country of origin France
Size
Height A: 18.95 m
B: 23.5 m
BP4: 21.6 m (A: 62.17 ft
B: 77 ft
BP4: 70.7 ft)
Diameter 1.34 m (4.39 ft)
Mass 18,400 kg (40,500 lb)
Stages 3
Capacity
Payload to LEO 160 kg (350 lb)
Launch history
Status Retired
Launch sites A: Hammaguir
B/BP4: Kourou
Total launches 12 (A :4, B: 5, BP4: 3)
Successes 9 (A: 3, B: 3, BP4: 3)
Failures 3 (A: 1, B: 2)
First flight A: 26 November 1965
B:10 March 1970
BP4:6 February 1975
Last flight A: 15 February 1967
B:21 May 1973
BP4: 27 September 1975
First stage (Diamant A) - Emeraude
Engines 4 Vexin B
Thrust 301.55 kN (67,791 lbf)
Specific impulse 221 sec
Burn time 93 seconds
Fuel N2O4/UDMH
First stage (Diamant B/BP4) - L-17
Engines 4 Vexin C
Thrust 396.52 kN (89,142 lbf)
Specific impulse 221 sec
Burn time 110 seconds
Fuel N2O4/UDMH
Second stage (Diamant A/B) - Topaze
Engines 1 Solid
Thrust 120.082 kN (26,996 lbf)
Specific impulse 255 sec
Burn time 39 seconds
Fuel Solid
Second stage (Diamant BP4) - P-4
Engines 1 Solid
Thrust 176 kN (39,566 lbf)
Specific impulse 273 sec
Burn time 55 seconds
Fuel Solid
Third stage (Diamant A) - P-6
Engines 1 Solid
Thrust 29.4 kN (6,609 lbf)
Specific impulse 211 sec
Burn time 39 seconds
Fuel Solid
Third stage (Diamant B/BP4) - P-6
Engines 1 Solid
Thrust 50 kN (11,240 lbf)
Specific impulse 211 sec
Burn time 46 seconds
Fuel Solid

The Diamant rocket (Diamant is French for "diamond") was the first exclusively French expendable launch system and at the same time the first satellite launcher not built by either the USA or USSR. As such it is the main predecessor of all subsequent European launcher projects. It was derived from the military program Pierres précieuses (fr.: gemstones) that included the five prototypes Agate, Topaze, Emeraude, Rubis and Saphir (Agate, Topaz, Emerald, Ruby and Sapphire). Design of the Diamant began in 1962, as the inaugural spacecraft project of France's space agency, the CNES. Out of 12 launch attempts between 1965 and 1975, 9 were successful. Most notably, the Diamant was used to put the first French satellite, Astérix, into orbit on November 26, 1965. Despite the success, France abandoned its national launcher program in favor of the European Ariane launcher in 1975.
Three successive versions of the Diamant rocket were developed, designated A, B and BP4. All versions had three stages and a payload of approximately 150 kg for a 200 km orbit.

Variants[edit]

Diamant A[edit]

This was the first version of the Diamant rocket. It was used to launch the Astérix and subsequently three other small satellites during 1965-67 from the base at Hammaguir in Algeria. Remarkably for a newly developed system, all four attempted launched were partly successful, the only failure occurring on the second launch when the payload was inserted into a lower orbit than planned. It possessed a first stage of 10 m, 1.4 metres in diameter, and a weight of 14.7 metric tons. Their engines of the type LRBA Vexin supplied a thrust of 269 kN for 93 seconds. The second stage was 4.7 metres long and had a diameter of 80 centimetres. It weighed 2.9 metric tons and developed a thrust of 165 kN for a duration of 44 seconds. The third stage of 2.65 m in diameter. Its weight amounted to 709 kilograms. It burned for 45 seconds and developed a thrust of 27 kN to 53 kN. Completely installed, a Diamond A was 18.95 metres high and weighed 18.4 metric tons.

Diamant B[edit]

An improved version of the Diamant A with a more powerful first stage. Five satellite launches were attempted between 1970 and 1973, of which the last two failed. All launches took place from Kourou in French Guyana, which thus became established as the sole French and European spaceport, a status that it still holds today (2013).

Its first stage was 14.2 meters long, had a diameter of 1.4 meters and weighed 20.1 metric tons. Its engine developed a thrust of 316 kN to 400 kN (as a function of the flight altitude) for 116 seconds. The second stage the Diamond B corresponded to that the Diamond A. The third stage was 1.67 meters long and had a diameter of 80 centimeters. It developed a thrust of 24 kN for 46 seconds. Completely assembled a Diamond B was 23.5 meters high and weighed 24.6 metric tons.

Diamant BP4[edit]

This version incorporated a new second stage, while carrying the first and third stages over from its predecessor. It performed three successful launches in 1975, putting a total of four satellites into orbit. Its second stage, which was derived from the MSBS rocket, was 2.28 metres long and 1.5 metres in diameter and developed a thrust of 180 kN for 55 seconds.

Launch History[edit]

Diamant flights
Date Variant Payload Launch Site Remarks Notes
November 26, 1965 Diamant A Asterix Algeria Hammaguir Success
February 17, 1966 Diamant A Diapason Algeria Hammaguir Success
February 8, 1967 Diamant A Diadème 1 Algeria Hammaguir Partial Failure Orbit too low
February 15, 1967 Diamant A Diadème 2 Algeria Hammaguir Success
March 10, 1970 Diamant B Mika / Wika France Kourou Success
December 12, 1970 Diamant B Péole France Kourou Success
April 15, 1971 Diamant B Tournesol France Kourou Success
December 6, 1971 Diamant B Polaire France Kourou Failed to orbit Second stage failed
May 21, 1973 Diamant B Castor / Pollux France Kourou Failed to orbit Fairing not separated
February 6, 1975 Diamant BP4 Starlette France Kourou Success
May 17, 1975 Diamant BP4 Castor / Pollux France Kourou Success
September 27, 1975 Diamant BP4 Aura France Kourou Success


See also[edit]


External links[edit]