Encyclopedia Astronautica
Jaguar



jaguar.jpg
Jaguar
The Jaguar was designed by the RAE Supersonics Department as part of the HRV (Hypersonic Research Vehicle) program. This was a joint project with the Australian Weapons Research Establishment for testing of re-entry vehicles at high speeds. Regardless of the variant, the Rook first stage would propel the upper stages and subscale RV to a high altitude. The upper stages would then fire downward to push the RV into the atmosphere at speeds of up to 5 km/s. After the conclusion of the HRV project in April 1970, tests continued using the Jabiru 3 with other aerothermal experiments until November 1974.

Success Rate: 100.00%. Launch data is: incomplete.

Status: Retired 1974.
First Launch: 1960.08.17.
Last Launch: 1974.11.20.
Number: 28 .

More... - Chronology...


Associated Countries
Associated Engines
  • Rook Royal Ordnance solid rocket engine. 300 kN. Out of production. Fast-burning version of Raven. Rook was fired 70 times altogether, in 65 flights and 16 different vehicle designs. More...

See also
  • Jaguar The Jaguar was designed by the RAE Supersonics Department as part of the HRV (Hypersonic Research Vehicle) program. This was a joint project with the Australian Weapons Research Establishment for testing of re-entry vehicles at high speeds. Regardless of the variant, the Rook first stage would propel the upper stages and subscale RV to a high altitude. The upper stages would then fire downward to push the RV into the atmosphere at speeds of up to 5 km/s. More...

Associated Manufacturers and Agencies
  • RAE British agency overseeing development of rockets and spacecraft. Royal Aerospace Establishment, UK. More...
  • WRE Australian manufacturer of rockets, spacecraft, and rocket engines. Australian Weapons Research Establishment, Australia. More...

Bibliography
  • McDowell, Jonathan, Jonathan's Space Home Page (launch records), Harvard University, 1997-present. Web Address when accessed: here.
  • Serra, Jean-Jacques, Rockets in Europe, Web Address when accessed: here.

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