Behavior of Extraction Parachutes in the Wake of a Powered Airplane Model.

Download this report (PDF, 1.87 MB, 102 pages)
Report Number: AFFDL TR 68-15
Author(s): Heinrich, Helmut G., Hulcher, G. D.
Corporate Author(s): Minnesota Univ Minneapolis Dept Of Aeronautics And Engineering Mechanics
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1968-08
Pages: 102
Contract: F33615-67-C-1010
DoD Project: 6065
DoD Task: 606503
Identifier: AD0842569

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

Provenance: Lockheed Martin Missiles & Fire Control

Other options for obtaining this report:

Via the Defense Technical Information Center (DTIC):
A record for this report, and possibly a pdf download of the report, exists at DTIC

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
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



Export