Abstract
The structure and concept of the reusable launch vehicle (RLV) is different from conventional satellite launch vehicles including its avionic systems architecture, which introduces new concept for power distribution and closed loop control response timings. This work describes about the systems involved in the testing of this new concept launch vehicle. The work also describes about the new avionic systems powering scheme introduced and new measurement system adopted.
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Schedule a callMore From: Journal of The Institution of Engineers (India): Series C
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