Record Details

Liquid propellant rocket combustion instability
NTRS Full-Text: Click to View  [PDF Size: 86.1 MB]
Author and Affiliation:
Harrje, D. T.(NASA, Washington, DC, United States)
Abstract: The solution of problems of combustion instability for more effective communication between the various workers in this field is considered. The extent of combustion instability problems in liquid propellant rocket engines and recommendations for their solution are discussed. The most significant developments, both theoretical and experimental, are presented, with emphasis on fundamental principles and relationships between alternative approaches.
Publication Date: Jan 01, 1972
Document ID:
(Acquired Nov 22, 1995)
Accession Number: 72N33729
Subject Category: PROPELLANTS
Report/Patent Number: NASA-SP-194
Document Type: Technical Report
Publisher Information: United States
Financial Sponsor: NASA; United States
Organization Source: NASA; Washington, DC, United States
Description: 657p; In English
Distribution Limits: Unclassified; Publicly available; Unlimited
Rights: No Copyright
› Back to Top
Facebook icon, External Link to NASA STI page on Facebook Twitter icon, External Link to NASA STI on Twitter YouTube icon, External Link to NASA STI Channel on YouTube RSS icon, External Link to New NASA STI RSS Feed
Find Similar Records
NASA Logo, External Link

NASA Official: Gerald Steeman

Sponsored By: NASA Scientific and Technical Information Program

Site Curator: STI Support Services

Last Modified: August 29, 2013

Privacy Policy & Important Notices Disclaimers, Copyright, Terms of Use Freedom of Information Act NASA OCIO Free Adobe PDF Reader Free MS Word Viewer