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・ August 1 Declaration
・ August 10
・ August 10 (Eastern Orthodox liturgics)
・ August 11
・ August 11 (Eastern Orthodox liturgics)
・ Augmented major seventh chord
・ Augmented matrix
・ Augmented ninth chord
・ Augmented octave
・ Augmented pentagonal prism
・ Augmented reality
・ Augmented Reality Assisted Surgery
・ Augmented Reality Assisted Urologic Surgery
・ Augmented Reality Markup Language
・ Augmented reality-based testing
Augmented Satellite Launch Vehicle
・ Augmented second
・ Augmented seventh
・ Augmented seventh chord
・ Augmented sixth
・ Augmented sixth chord
・ Augmented sphenocorona
・ Augmented third
・ Augmented transition network
・ Augmented tree-based routing
・ Augmented triad
・ Augmented triangular prism
・ Augmented tridiminished icosahedron
・ Augmented truncated cube
・ Augmented truncated dodecahedron


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Augmented Satellite Launch Vehicle : ウィキペディア英語版
Augmented Satellite Launch Vehicle

|status = Retired
|first = 24 March 1987
|last = 4 May 1994
|launches = 4
|success = 1
|fail = 2
|partial = 1
|sites = Sriharikota
|family = SLV, Polar Satellite Launch Vehicle, GSLV
|payloads = SROSS
|stagedata =





}}
The Augmented Satellite Launch Vehicle'' or Advanced Satellite Launch Vehicle, also known as ASLV, was a five-stage solid-fuel rocket developed by the Indian Space Research Organisation (ISRO) to place 150 kg satellites into LEO.〔(【引用サイトリンク】 title=ASLV )〕 This project was started by India during the early 1980s to develop technologies needed for a payload to be placed into a geostationary orbit.〔http://www.bharat-rakshak.com/SPACE/space-launchers-aslv.html〕 Its design was based on Satellite Launch Vehicle.〔http://www.astronautix.com/lvs/aslv.htm〕 ISRO did not have sufficient funds for both the Polar Satellite Launch Vehicle programme and the ASLV programme at the same time and the ASLV programme was terminated after the initial developmental flights.〔 The payloads of ASLV were Stretched Rohini Satellites.〔
==Vehicle==
The ASLV was a five-stage vehicle. Two strap-on boosters acted as a first stage, with the core stage igniting after booster burn out. The payload capacity of the ASLV was approximately 150 kg to an orbit of 400 km with a 47-degree inclination.〔
At liftoff, the ASLV generated 92,780 kgf of thrust. It was a 41,000 kilogram rocket, measuring 23.5 metres in length with a core diameter of one metre.〔

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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