Analysis of performance of a hot gas injection thrust vector controlsystem
Author:
Affiliation:
1. Vikram Sarabhai Space Centre, Trivandrum, 695022 India
2. Indian Institute of Science, Bangalore, 56012 India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.23365
Reference11 articles.
1. On secondary gas injection in supersonic nozzles.
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