Chugging Instability of H2O2 Monopropellant Thrusters with Reactor Aspect Ratio and Pressures

Title
Chugging Instability of H2O2 Monopropellant Thrusters with Reactor Aspect Ratio and Pressures
Authors
Keywords
-
Journal
JOURNAL OF PROPULSION AND POWER
Volume 27, Issue 2, Pages 422-427
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Online
2011-03-22
DOI
10.2514/1.48939

Ask authors/readers for more resources

Find Funding. Review Successful Grants.

Explore over 25,000 new funding opportunities and over 6,000,000 successful grants.

Explore

Discover Peeref hubs

Discuss science. Find collaborators. Network.

Join a conversation