This paper describes the results of current research being carried out at McDonnell Douglas Aerospace (MDA) to develop a flight-ready vibration isolation system for possible use on shuttle or space station. Measurements and predictions indicate that the natural vibration modes of these vehicles may be excited by on-board equipment and astronaut activities. These disturbances may be enough to upset the desired levels of microgravity. The MDA system consists of a very low frequency, flexible interface between a scientific payload and the orbiting host platform augmented by active acceleration feedback. The design of a system that will accommodate materials and biological experiments must take into account predicted input vibration levels, experiment services requirements, and logistic considerations. It must accommodate all these requirements while consuming the absolute minimum of the space available to the payload itself. The MDA isolator concept has been demonstrated in 3-axis testing in the laboratory and nearly meets the desired space station specifications. However, the design needs on-orbit testing to verify its performance in true space environment. This paper discusses some of the practical aspects of the design and operation of the system. NASA has notified MDA that a Phase A award for the development of a flight demonstration of our experiment will be made under its IN-Space Technology Experiment Program (IN-STEP).
Ground testing of a microgravity isolation system
Smart Structures and Materials 1994: Smart Structures and Intelligent Systems ; 1994 ; Orlando,FL,United States
Proc. SPIE ; 2190
1994-05-06
Conference paper
Electronic Resource
English
A microgravity isolation mount
NTRS | 1987
|Microgravity Vibration Isolation Mount
British Library Conference Proceedings | 1994
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