Please make a donation to support Gunter's Space Page.
Thank you very much for visiting Gunter's Space Page. I hope that this site is useful and informative for you.
If you appreciate the information provided on this site, please consider supporting my work by making a simple and secure donation via PayPal. Please help to run the website and keep everything free of charge. Thank you very much.


Wresat [WRE]

Wresat (Weapons Research Establishment Satellite), built within 11 months by the Australian Weapons Research Establishment, was launched by a surplus Redstone Sparta launch vehicle from Woomera into a 198 km × 1252 km orbit inclined at 83 deg. The 45 kg Australian microsatellite transmitted for 5 days. It reentered after 42 days.

The battery powered Wresat carried four experiments, which were derived from experiments flown on earlier australian sounding rockets:

  • Solar UV (1050 Å-1660 Å)
  • Solar UV (2500 Å)
  • Geocoronal Hydrogen Lyman Alpha
  • Solar X-Ray (8 Å)

As such, these sensors were predominantly for upper atmospheric research. There were sensors to measure solar radiation, specifically three wavelengths which had the greatest impact on the temperature and composition of the upper atmosphere. The same sensors could also measure the temperature of the solar atmosphere and the density of molecular oxygen in the Earth's atmosphere. Additionally, there was a small telescope with a lithium fluoride lens which could measure the faint ultraviolet halo (GeoCoronal) that surrounds the Earth at night.

For simplicity, the satellite was integrated directly into the SPARTA third stage. WRESAT was a little over two meters long and weighed approximately 72.5 kg, including the burned out rocket motor.

The satellite was launched on 29 November 1967 on a Redstone Sparta from Woomera into an excentric elliptical polar orbit of 198 km × 1252 km with an inclination of 83.3. WRESAT operated for two weeks until the batteries ran out of power. WRESAT re-entered the atmosphere on 10 January 1968 after 43 days in orbit and burned up.

Nation: Australia
Type / Application: Technology
Operator: Australian Weapons Research Establishment (WRE)
Contractors: Australian Weapons Research Establishment (WRE)
Configuration: Cone
Propulsion: None
Power: Batteries
Lifetime: 5 days
Mass: 45 kg; 72 kg including the integrated 3rd stage
Orbit: 198 km × 1252 km, 83.3
Satellite COSPAR Date LS Launch Vehicle Remarks
Wresat 1967-118A 29.11.1967 Wo LA-8 Redstone Sparta

Cite this page: