Electromagnetic Steering of Sodium-Seeded Rocket Thrust Plumes: Design & Analysis
This paper explores the use of the Lorentz force to magnetically steer a rocket engine’s thrust plume, creating an off-axis thrust component. The perpendicular force component thus generated, for the sample design used is estimated at 0.002% without sodium seeding, and 3.5% with said seeding. The de...
Main Author: | Gershon, Levi |
---|---|
Other Authors: | Hart, Douglas |
Format: | Thesis |
Published: |
Massachusetts Institute of Technology
2023
|
Online Access: | https://hdl.handle.net/1721.1/150153 https://orcid.org/0000-0001-7700-9570 |
Similar Items
-
Liquid rocket thrust chambers : aspects of modeling, analysis, and design /
by: Yang, Vigor
Published: (2004) -
S rocket thrust sensor as a gravity sensor /
by: Mohd. Faizal Zakaria, 1989-, et al.
Published: (2012) -
The use of swirl to clean nuclear rocket plumes
by: Oh, David Y. (David Younghee)
Published: (2009) -
Life Analysis of Reusable Liquid Rocket Engine Thrust Chamber
by: Yuanjie Qi, et al.
Published: (2022-12-01) -
Thrust Control Method and Technology of Variable-Thrust Liquid Engine for Reusable Launch Rocket
by: Zhaohui Yao, et al.
Published: (2022-12-01)