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Configuration and Design of Checkout System for Reusable Launch Vehicle

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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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Authors and Affiliations

  1. Vikram Sarabhai Space Centre, Indian Space Research Organisation, Thiruvananthapuram, India

    A. Muraleedharan, V. Mohanan Chettiar, U. Shyamkumar, V. Vivekanand, C. R. Sandeep & V. Kishorenath

Authors
  1. A. Muraleedharan
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  2. V. Mohanan Chettiar
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  3. U. Shyamkumar
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  4. V. Vivekanand
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  5. C. R. Sandeep
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  6. V. Kishorenath
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Corresponding author

Correspondence to V. Vivekanand.

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Muraleedharan, A., Mohanan Chettiar, V., Shyamkumar, U. et al. Configuration and Design of Checkout System for Reusable Launch Vehicle. J. Inst. Eng. India Ser. C 98, 649–656 (2017). https://doi.org/10.1007/s40032-017-0408-4

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  • DOI: https://doi.org/10.1007/s40032-017-0408-4

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