In-Flight Simulation of the Lateral-Directional Handling Qualities of Entry Vehicles

Item

Title
In-Flight Simulation of the Lateral-Directional Handling Qualities of Entry Vehicles
Date
1961
Index Abstract
Coming Soon
Photo Quality
Not Needed
Report Number
WADD TR 61-147
Corporate Author
Cornell Aeronautical Laboratory, Inc.
Laboratory
Flight Control Laboratory
Extent
65
Identifier
AD0269517
AD0269517
Access Rights
OTS
Distribution Classification
1
Contract
AF 33(616)-5823
DoD Project
8219
DoD Task
82163
DTIC Record Exists
Yes
Distribution Change Authority Correspondence
None
Abstract
The initial results of a flight research program to simulate the handling qualities of winged vehicles during atmospheric entry are discussed. The purpose is to evaluate in flight the effects on pilot-vehicle performance of the dynamic flight characteristics of atmospheric entry vehicles, and to determine their suitability for the entry mission. The evaluations were conducted in a three-axis variable stability T-33 airplane. Different sets of handling characteristics were evaluated in maneuvering flight and rated as to their suitability for the entry mission. Emphasis was placed upon the lateral handling characteristics, and 129 configurations were examined by one pilot. An effort is made to relate pilot objections and the attendant poor ratings to their causative vehicle characteristics. The piloting difficulties involved in the control of vehicles with either static or dynamic directional instabilities are discussed.
Report Availability
Full text available
Date Issued
1961-11
Publisher
Wright-Patterson Air Force Base, OH : Aeronautical Systems Division, Air Force Systems Command, United States Air Force
Date Modified
Scanned by request submitted 12/23/2019 by Massachusetts Institute of Technology (University - Domestic)
AD Number
AD269517
Provenance
AFRL/VACA
Type
report
Format
1 online resource
Creator
Harper, Robert P.