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Space Projects

 

KISTLER LAUNCH VEHICLE

Analysis of the external vibro-acoustic environment by Vipac of the Kistler Launch Vehicle led to predictions of internal vibration levels.
Vipac worked on the development of the Kistler re-usable Launch Vehicle to place small satellites into a low Earth Orbit. Our role on this project involved:
  • Definition of the vibro-acoustic environment to be experienced by the vehicle
  • Assessment of vibration levels by internal equipment and payload
  • Investigation of the potentially key issue of failure/fatigue of critical components
  • Lift-off loads summary
  • Launch pad considerations with respect to acoustic environment


    FEDSAT MICRO- SATELLITE

    Vipac's responsibility for the FedSat platform includes payload qualifications for the launch and space environments
    As a core member of the Co-Operative Research Centre for Satellite Systems (CRCSS), Vipac has a pivotal role in the current FedSat Project. With overall responsibility for the FedSat platform, Vipac's specific tasks include:
  • Development of the bus
  • Definition of payload/structure interfaces
  • System level responsibility for mechanical & structural systems
  • Assembly, Integration and Test of the platform

    This is an aggressive programme with launch scheduled for late 2000 on the Japanese HIIA rocket, and requires constant coordination with other CRC members and international suppliers. Payloads include instrumentation to measure the Earth's magnetic field and to demonstrate the use of high speed computers in space environments.

    ATMOSPHERIC PRESSURE SENSOR

    With the CSIRO, Vipac has developed a Fabry Perot optical Configuration for the APS suitable for space based platforms.
    The APS is a satellite-based instrument for measuring atmospheric pressure at the sea surface. In conjunction with CSIRO/DAR, Vipac managed a Phase A study to produce a demonstrator prototype which underwent successful trials on an F27 aircraft. Vipac also undertook the design, development and implementation of an alternative lightweight space instrument which is now the baseline for a space engineering development programme.