首页> 外文期刊>Journal of the British Interplanetary Scoiety >De Havilland Rocket Engines: Part 2* - The Sprite Rocket Engine: Catalyst Packs, Kerosene and the Comet Trials
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De Havilland Rocket Engines: Part 2* - The Sprite Rocket Engine: Catalyst Packs, Kerosene and the Comet Trials

机译:De Havilland火箭发动机:第2部分*-Sprite火箭发动机:催化剂包,煤油和彗星试验

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Early in 1947 the de Havilland Special Projects Group, led by Val Cleaver, started work on their first project the Sprite rocket engine [1]. Officially given the Ministry of Supply [MOS] designation D. Sp.1 the Sprite was a fairly simple 'cold' hydrogen peroxide engine using liquid permanganate as a catalyst. The engine was intended as a rocket assisted take off [RATO] unit for the Comet jet airliner. Such a requirement was deemed necessary because it was thought that the early Ghost jet engines would need rocket take off assistance at 'hot and high' airfields such as Khartoum and Nairobi. The very first firing of the D.Sp.l Sprite rocket engine was carried out at Hatfield on 24 November 1949. However by the spring of 1950 it had become clear that the Ghost 50 Mk 1 engines, which powered the Comet 1, had performed better than expected during trials at tropical airfields. Consequently the Sprite was no longer required for its intended purpose.
机译:1947年初,由Val Cleaver领导的de Havilland特别项目小组开始了他们的第一个Sprite火箭发动机项目的工作[1]。 Sprite官方指定为供应部(MOS)的名称D. Sp.1,它是一种相当简单的“冷”过氧化氢发动机,使用液态高锰酸盐作为催化剂。该发动机旨在作为彗星喷气客机的火箭辅助起飞[RATO]单元。之所以认为这一要求是必要的,是因为人们认为,早期的Ghost喷气发动机将需要在喀土穆和内罗毕这样的“高温高空”机场起飞的火箭协助起飞。 1949年11月24日,D.Sp.l Sprite火箭发动机首次点火在哈特菲尔德进行。但是,到1950年春天,很明显,为彗星1发动机提供动力的Ghost 50 Mk 1发动机已经执行了在热带机场进行的试验中比预期的要好。因此,Sprite不再需要用于其预期的目的。

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