F-111D, DT and E Evaluation of Environmental Control, Airframe, Flight Control, and Secondary Power Subsystems. Appendix 1

During the arctic test phase of the F-111D DT/E All-Weather Test Program, 24.0 hours of test time were accumulated in 12 test flights. Five of these flights were selected as being most representative of aircraft operation in an arctic environment. All available data obtained on these five flights ar...

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Bibliographic Details
Main Author: Olson, Richard W
Other Authors: AIR FORCE TEST CENTER EDWARDS AFB CA
Format: Text
Language:English
Published: 1973
Subjects:
Bombers
Attack and Fighter Aircraft
*JET FIGHTERS
AIRFRAMES
ARCTIC REGIONS
AVIONICS
CHECKOUT PROCEDURES
COCKPITS
COLD WEATHER TESTS
COMPUTER PRINTOUTS
COOLING AND VENTILATING EQUIPMENT
DATA PROCESSING
DEICING SYSTEMS
ENVIRONMENTAL TESTS
FIGHTER BOMBERS
FLIGHT CONTROL SYSTEMS
FLIGHT TESTING
HEATING
HYDRAULIC EQUIPMENT
PERFORMANCE(ENGINEERING)
TEMPERATURE
F-111D AIRCRAFT
*F-111 AIRCRAFT
Arctic
Online Access:http://www.dtic.mil/docs/citations/ADB002373
http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=ADB002373
Description
Summary:During the arctic test phase of the F-111D DT/E All-Weather Test Program, 24.0 hours of test time were accumulated in 12 test flights. Five of these flights were selected as being most representative of aircraft operation in an arctic environment. All available data obtained on these five flights are presented in this document as computer printouts. Appendix 1 to ADB002372. See also Appendix 2, ADB002374.

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