Vertical Landing Rockets

Authors

  • Sucheth Krishna Kumar Bysani
  • Anoop Karpur
  • Nirnay Arun

Keywords:

vertical landing vehicle, retropropulsive landings, RCS (reaction control system), GPS, grid fins, thrust vector control, Cold gas thrusters, deployable landing gear, terrain mapping

Abstract

The concept of Vertical landing Rockets was developed to achieve re-usability of the rocket in order to decrease cost and time of Rocket launching. Successful attempts of vertical landing rockets have been attempted by SpaceX and Blue origin with the motivation of reduction of manufacturing and research costs, these have led the path for the re-usability of rocket engines and autonomous recovery of rockets. This paper will discuss the challenges to meet the precision landing of rockets on earth and other planets and also factors required to extend this technology to implement it in future space tourism.

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Published

2020-01-20

How to Cite

1.
Kumar Bysani SK, Karpur A, Arun N. Vertical Landing Rockets. ExCon [Internet]. 2020 Jan. 20 [cited 2024 Dec. 30];8(4):33-4. Available from: https://wcc.ep.liu.se/index.php/TMAL02/article/view/555

Issue

Vol. 8 No. 4 (2019): Proceedings of the 4th TMAL02 Expert Conference, October 14, 2019, Linköping University, Linköping, Sweden

Section

Supersonic & Space