New Propulsion Concepts Based on New Cycles

Item

Title
New Propulsion Concepts Based on New Cycles
Description
This paper examines the typical interrelationship amongst the engine, the aircraft, and the mission requirements to determine the probable future trends in new airbreathing propulsion cycles. Engine concepts employing multiple cycle, or multi-mode capability within a single engine are identified and their future potential defined. Examples are described in terms of recent results from feasibility research programs on several multi-mode engine concepts. The paper covers both aircraft and missile propulsion systems for the future.
Creator
Fisher, R. E.
Publisher
Arlington, VA : Air Force Office of Scientific Research
Date
1969
Format
3 pages ; 28 cm.
Type
article
Abstract
This paper examines the typical interrelationship amongst the engine, the aircraft, and the mission requirements to determine the probable future trends in new airbreathing propulsion cycles. Engine concepts employing multiple cycle, or multi-mode capability within a single engine are identified and their future potential defined. Examples are described in terms of recent results from feasibility research programs on several multi-mode engine concepts. The paper covers both aircraft and missile propulsion systems for the future.
Date Issued
1969-12
Corporate Author
Marquardt Corporation, Aerospace Products Division
Report Number
AFOSR 69-2951TR p. 76-78
Distribution Conflict
No
Index Abstract
Contrails only
Photo Quality
Not Needed
Distribution Classification
1
DTIC Record Exists
Yes
Report Availability
Full text available by request
Identifier
AD0703442