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RTV1


General Information

The Research Test Vehicle (RTV) 1e was developed and tested at the Woomera Rocket Range in South Australia by Fairey Aviation. The RTV 1e was a two-stage liquid fuel rocket used for research and development into problems associated with beam riding missiles. It was fired at an angle of 35 degrees with a maximum altitude of about 12,000 feet. The RTV 1e was launched by seven solid booster rockets which had a burn time of four seconds, after which the liquid fuel sustainer motor took over.



Purpose:
Period of Use:
Payload Mass: 12,000 ft
Apogee:

Motor Details

Ignition Motor Impulse Burn Time
Stage 1 T+0


Launch Log


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