Parameter Analysis To Develop A Practical Thrustmeter System Of The J79 Phase I Turbojet Engine

This citation is provided as a resource for researchers, but Contrails cannot provide a full-text download

U.S. government employees, Military/Department of Defense employees, and U.S. government contractors and sub-contractors may be eligible to register with the Defense Technical Information Center (DTIC), where this report and others like it may be available
Report Number: WADC TR 59-54
Author(s): Chase, R. E., Elgin, J. A., Fischer, M. A.
Corporate Author(s): General Electric Company.
Date of Publication: 1959-05
Pages: 62
DoD Task:
PB Number: PB156284

Abstract:
The abstract for this report is either unavailable or has yet to be entered

Other options for obtaining this report:

Via the Defense Technical Information Center (DTIC):
This report may be available for download from DTIC
Use the Title from this record to locate the item in DTIC Online

Via National Technical Report Library:
This report may be available for download from NTRL. Use the Title from this record to locate the item in DTIC Online

Indications of Public Availability
A PB Number, PB156284 , exists for this report, indicating public availability of the report at time of publication

No digital image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement