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The ALV system uses between one and six boosters connected to a core. The boosters each have a V-tail system that, on launch, act as stabilising fins; during the return flight and landing, the V-tail provides directional control. After first stage separation, the boosters coast (ballistic cruise).
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After re-entry, at around 350 km down range, the wings deploy and the boosters manoeuvre for return flight to the launch site, using a deployable propeller driven by an engine, acting as a large
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The Second Stage core flies on after First Stage booster separation, with the stack. The core separates and returns to the atmosphere and Earth and is not recovered.
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After fairing separation, the Third Stage and
Payload fly to orbit. Payload separation is as required for the mission. Third Stage deorbits and burns up on entry.
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Flight tests were scheduled for late in 2015. The first successful flight of the ALV was completed on 23 December 2015.
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The
Austral Launch Vehicle: Reducing Space Transportation Cost Through Reusability, Modularity And Simplicity
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University of
Queensland - Faculty of Engineering, Architecture and Information Technology
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77:(ALV) is a concept for a re-usable launch vehicle first stage. It would use fly-back
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The race is still on for a reusable rocket despite the SpaceX setback
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272:"UQ system set to launch Australia into space"
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89:The ALV concept is being developed by
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333:Space launch vehicles of Australia
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313:Heliaq Advanced Engineering
160:University of Queensland's
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306:Professor Michael Smart
208:Australian Space Agency
38:, as no other articles
343:Proposals in Australia
75:Austral Launch Vehicle
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278:. 24 December 2015
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62:October 2015
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118:First stage
322:Categories
282:24 January
214:References
103:Queensland
85:Proponents
53:; try the
40:link to it
162:SPARTAN-1
43:. Please
172:See also
165:scramjet
99:Brisbane
93:and the
276:UQ News
167:project
147:Testing
113:System
36:orphan
34:is an
97:from
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73:The
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79:UAV
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