Encyclopedia Astronautica
HAT-1


Solid propellant rocket stage. Loaded mass 300 kg.

No Engines: 2.

Status: Retired 1963.
Gross mass: 300 kg (660 lb).
Height: 1.80 m (5.90 ft).
Diameter: 0.41 m (1.34 ft).

More... - Chronology...


Associated Countries
Associated Engines
Associated Launch Vehicles
  • HAT Australian test vehicle. Two stage vehicle consisting of 1 x HAT + 1 x LAPSTAR More...

Associated Manufacturers and Agencies
  • WRE Australian manufacturer of rockets, spacecraft, and rocket engines. Australian Weapons Research Establishment, Australia. More...

Associated Propellants
  • Solid Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. More...

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