MarketDiamant
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Diamant

The Diamant rocket was the first exclusively French expendable launch system and at the same time the first satellite launcher not built by either the United States or USSR. As such, it has been referred to as being a key predecessor for all subsequent European launcher projects. The head of the project, Charley Attali, received the Legion of Honour in 1965 for the Diamant.

Development
Background During the late 1940s and 1950s, substantial interest arose amongst the international powers of the era in the development of rocketry and missile technology, in particular the prospects for ballistic missiles capable of travelling great distances. Both of the emergent superpowers of the time, the United States and the Union of Soviet Socialist Republics (USSR) chose to invest heavily within this new field, observing its political and military importance; it was not long before a highly competitive atmosphere emerged where neither entity wished to fall behind the other in missile technology, which directly led to the so-called 'space race'. In addition, other nations also sought to make headway with this technology, often seeking to exploit and build upon knowledge which had been acquired from Nazi Germany's V2 programme. In western Europe, both the United Kingdom and France began making significant early steps in this field. During 1949, the French government established the Laboratoire de Recherches Balistiques et Aérodynamiques at Vernon, outside Paris, for the purpose of pursuing its own military-focused ballistic missiles programmes. The agency initially conducted relatively straightforward and cost-conscious programmes, such as the development of the V2-based Veronique liquid-fuelled rocket in cooperation with a number of German scientists, which first flew during 1954. During 1957, having been suitably encouraged by the progress made, the Comité d'Action Scientifique de Défense Nationale (CASDN) decided to finance further refinements of the Veronique rocket. During 1958, French wartime military leader Charles de Gaulle became President of France, establishing the Fifth Republic. This maiden flight was deemed to be a success, achieving sufficient altitude and launching French's first satellite, a 42 kg test vehicle known as Astérix, into orbit; this feat has been viewed as cementing France as the third space power in the world, as well as affirming its independence and strategic capabilities. During 1966 and 1967, Diamant was used to launch three French-built scientific satellites. On 10 March 1970, the first Diamant B rocket, an improved model of the launcher, was fired, carrying a pair of scientific satellites, named DIAL/MIKA and DIAL/WIKA, into orbit. Overall, the Diamant rocket came to be recognised as a successful and reliable launch vehicle, competitive amongst even the best of its international competitors throughout the world during its time. Successor and discontinuation While Diamant had proven to be a viable and reliable launcher, the sheer size of the American and Soviet space programmes far exceeded what would be realistically achievable not only by France but by any of the independent nations of western Europe. As a consequence of Britain's withdrawal from participation in the ELDO, it was decided to replace the British-built Blue Streak, which comprised the first stage of the organisation's multinational launcher, known as Europa, with the French-built Diamant taking its place. All work on the Europa programme was terminated only a few years later due to the high failure rate encountered. Meanwhile, Britain decided to focus its efforts on the indigenous Black Arrow launcher instead. During 1974, the European Space Agency (ESA) was founded for this purpose; the ESA effectively enabled the competing and overlapping national space programmes to be succeeded by a single organised multinational framework with work shared between the member states instead. Specifically, in 1976, work commenced on the new collaborative Ariane 1 launcher, the first version of what would become the highly successful Ariane family. The existence of the Ariane programme, a rival launcher to the earlier Diamant rocket, effectively replaced the demand for and the role of France's indigenous launcher, rendering it obsolete and redundant in comparison. France ultimately decided to discontinue further launches using Diamant in favour of the newer Ariane platform. == Variants ==
Variants
Diamant A in Musée de l'Air This was the first version of the Diamant rockets, operational between 1965 and 1967. Remarkably for a newly developed system, all of the first four launches attempted launched were partly successful, the only failure occurring on the second launch when the payload was inserted into a lower orbit than planned. Completely assembled, a Diamant A was 18.95 metres high and weighed 18.4 metric tons. The first stage had a Vexin B nitric acid/turpentine engine supplying a thrust of 274 kN for 93 seconds. Five satellite launches were attempted between 1970 and 1973, of which the last two failed. All launches took place from Kourou in French Guiana. Completely assembled, a Diamant B was 23.5 metres high and weighed 26.9 metric tons. Its Améthyste first stage was 14.2 meters long, had a diameter of 1.4 metres and weighed 20 metric tons. Its LRBA Valois N2O4/UDMH engine developed a thrust of 315 kN for 116 seconds. The Topaze P-2.2 second stage had one P4 solid propellant engine that developed a thrust of 150 kN for a duration of 44 seconds. The P06 third stage was 1.66 metres long and had a diameter of 80 centimetres. Its P0.68 solid propellant engine developed a thrust of 50 kN for 46 seconds. Diamant BP4 This version incorporates 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. Completely assembled, a Diamant BP4 measured 22.68 metres high and weighed 20.3 metric tons. Its Rita P-4 second stage, which was derived from the MSBS rocket, was 2.28 metres long, 1.51 metres in diameter and its P4 solid propellant engine developed a thrust of 176 kN for 55 seconds. == Launch history ==
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