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A high-performance 250-pound-thrust rocket engine utilizing coaxial-flow injection of JP-4 fuel and liquid oxygen

By Stein, Samue

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Book Id: WPLBN0002207750
Format Type: PDF eBook :
File Size: 1.1 MB
Reproduction Date: 2012

Title: A high-performance 250-pound-thrust rocket engine utilizing coaxial-flow injection of JP-4 fuel and liquid oxygen  
Author: Stein, Samue
Volume:
Language: English
Subject: F-86 AIRCRAFT, PITCHING MOMENTS, FLOW CHARACTERISTICS
Collections: NASA Publication Collection
Historic
Publication Date:
1959
Publisher:

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Samue, S. (1959). A high-performance 250-pound-thrust rocket engine utilizing coaxial-flow injection of JP-4 fuel and liquid oxygen. Retrieved from http://worldpubliclibrary.org/


Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents

Summary
Contributor: National Aeronautics and Space Administration (NASA). The digitalization of this book was sponsored by National Aeronautics and Space Administration (NASA); Additional Subject Descriptions: F-86 AIRCRAFT; PITCHING MOMENTS; FLOW CHARACTERISTICS; AERODYNAMIC CHARACTERISTICS; THRUST REVERSAL; WIND TUNNEL TESTS; PERFORMANCE PREDICTION

 

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