The Australian Space Research Institute (ASRI) was formed 1991 with the merger of the AUSROC Launch Vehicle Development Group at Monash University, Melbourne and the Australian Space Engineering Research Association (ASERA).

The institute is a non-profit organisation run entirely by volunteers. Most of the work at ASRI is done in collaboration with Australian universities such as the Royal Melbourne Institute of Technology, Queensland University of Technology and the University of Technology, Sydney. , ASRI is developing a vision for the future of Australia's space community, including industry. ASRI does not receive any direct government funding.

Australian Space Research Institute

The ASRI was created to provide opportunities for space-related industry and technology development for the Australian technical community.

Australian Space Research Institute

History of space activities in Australia

During the heyday of rocketry research in the 1960s Australia was the seventh nation to launch a satellite, WRESAT, into orbit, and the third from its own soil.

Australian Space Research Institute

The joint British-Australian Blue Streak program to develop Intercontinental ballistic missiles ended in the late 1960s.

Around the same time the European Launcher Development Organisation (ELDO) was established to develop a European satellite launch vehicle. Woomera, Australia, was chosen as the launch site for the test vehicles. Australia was granted status as the only non-European member of ELDO (one of the precursors to the European Space Agency) in return for providing the launch facilities. A series of successful launches was conducted from 1964 to 1970 with the aim of reaching orbit and eventually orbiting an operational satellite. The final launch attempt of ELDO's Europa 1 launch vehicle took place at Woomera on 12 June 1970 however the satellite failed to reach orbit. No successful satellite launch was ever achieved by the ELDO and European satellite launch activities then shifted to the French site at Kourou, in French Guiana, which is now home to Ariane launchers.

Since then Australian space-related activities have been virtually nonexistent. The goal of the ASRI is to re-establish Australia as a significant player in the global space industry.

Sounding Rockets

The Small Sounding Rocket Program (SSRP), initiated in the mid-1990s, provides Australian educational institutions with a low cost payload launch service. The service has expanded to include individuals, companies, foreign universities and non-commercial organisations seeking assistance to launch their own vehicles.

Launches are conducted twice a year from Woomera, South Australia. Two types of rockets are used: Sighter, a solid fuel rocket capable of launching a 3 kg payload to an altitude of 5.9 km at speeds over Mach 1, and Zuni, a solid fuel rocket capable of launching a heavier payload to an altitude of approximately 7 km, and reaching speeds of Mach 2.5.

Launch vehicle development

The aim of the AUSROC program is to develop a micro-satellite launch vehicle capable of being scaled up for use in heavier launch vehicles.

AUSROC I

The AUSROC I program commenced in 1988 with a group of undergraduate students in Mechanical Engineering at Monash University, who designed and built AUSROC I. It was successfully launched on 9 February 1989. The flight lasted one minute, reaching 3 km in altitude and 161 m/s. AUSROC I was a liquid-fueled rocket based on a modified Pacific Rocket Society design.

AUSROC II

AUSROC II was a larger pressure fed kerosene-oxygen bipropellant rocket that was developed in the 1990s. It was designed to reach an altitude of 10 km. The first attempt at launching an AUSROC II suffered a spectacular failure on the launch pad in 1992. The subsequent rocket, named AUSROC II-2 was successfully launched in 1995 from Woomera, although it did not reach its target apogee due to pressurisation problems with the LOX tank.

AUSROC 2.5

AUSROC 2.5 was designed to provide an intermediate step between the AUSROC II and III programs. It uses the same size engine as the AUSROC III but with simpler and easier to implement cooling methods. The primary objective was to deliver a 10 kg payload to an altitude of 20 km and recover the rocket intact.

AUSROC 2.5 was the principal subject of current developments efforts. It was projected to launch in late 2007. Prior to that, a key milestone was the ground testing of the propulsion subsystem.

The project is currently seeking volunteers to assist with manufacturing, integration and testing.