The HAD rocket
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| '''Back''' to [[WRE HAD Rocket Experiments]] | '''Back''' to [[WRE HAD Rocket Experiments]] | ||
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| [[Image:HAD-rocket.jpg|right|thumb|HAD rocket: Diag - Ref. 1]] | [[Image:HAD-rocket.jpg|right|thumb|HAD rocket: Diag - Ref. 1]] | ||
| The two-stage HAD rocket consisted of a '''Gosling boost motor''' with a '''LAPstar rocket''' as its second stage, | The two-stage HAD rocket consisted of a '''Gosling boost motor''' with a '''LAPstar rocket''' as its second stage, | ||
Revision as of 01:51, 14 February 2007
Back to WRE HAD Rocket Experiments
The two-stage HAD rocket consisted of a Gosling boost motor with a LAPstar rocket as its second stage,
The term ‘LAPSTAR’ is used fairly loosely In Fire Across the Desert and is quoted this way on page 403 and a number of other instances. Light Alloy Plastic (LAP) motors were developed in the UK in 1938 and the surplus motors were transported to Woomera after WWII when the Joint Project was set up in the late 1940's. The motors were used on the RTV series of rockets which were the first launched from Woomera. The propellant was 'extruded double base' commonly known as cordite.
When Australia began to manufacture its own solid rocket motors at Maribyrnong in the 1960's in support of the Upper Atmospheric Research program, cordite as a rocket motor propellant was obsolete and we moved on to composite propellants consisting of aluminium powder, ammonium perchlorate, a rubber binder and a catalyst; with a better performance and longer shelf life.
The name LAP was retained from 1938 and the "star" was added as this was the profile of the propellant grain; hence the name LAPstar.
These further notes provided by Bruce Henderson, 13 February 2006
