Author :
Publisher :
Page : 4 pages
File Size : 31,99 MB
Release : 1971
Category : Aeronautics
ISBN :
[PDF] Inflight Emergency Escape Systems Aircraft Requirements For eBook
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In-flight Escape Systems for Helicopters Should be Developed to Prevent Fatalities
United States. General Accounting Office
Author : United States. General Accounting Office
Publisher :
Page : 36 pages
File Size : 42,5 MB
Release : 1973
Category : Aircraft survival equipment
ISBN :
Capsule Emergancy Escape Systems
U.S. Army Natick Research, Development, and Engineering Center
Author : U.S. Army Natick Research, Development, and Engineering Center
Publisher :
Page : 41 pages
File Size : 32,34 MB
Release : 1970
Category : Parachutes
ISBN :
This specification covers the requirements for capsule-type emergency escape systems for use on aircraft capable of exceeding 600 knots equivalent airspeed (KE AS) or altitudes of 50,000 feet.
Report to the Congress: In-flight Escape Systems for Helicopters Should be Developed to Prevent Fatalities
United States. General Accounting Office
Author : United States. General Accounting Office
Publisher :
Page : 36 pages
File Size : 32,57 MB
Release : 1973
Category : Aircraft survival equipment
ISBN :
Cartridge Actuated Devices, Aircraft Crew Emergency Escape General Specification for
Air Force Flight Dynamics Laboratory (U.S.)
Author : Air Force Flight Dynamics Laboratory (U.S.)
Publisher :
Page : 26 pages
File Size : 24,61 MB
Release : 1957
Category : Aeronautics
ISBN :
This specification establishes the general requirements that are common to cartridge actuated devices used in aircraft crew emergency escape systems.
Aircraft Emergency Escape System, Identification of
Author :
Publisher :
Page : 20 pages
File Size : 46,70 MB
Release : 1964
Category :
ISBN :
United States Army Aviation Digest
Author :
Publisher :
Page : 624 pages
File Size : 29,15 MB
Release : 1974
Category : Aeronautics
ISBN :
Capsule Emergency Escape System, General Requirements for
Air Force Flight Dynamics Laboratory (U.S.)
Author : Air Force Flight Dynamics Laboratory (U.S.)
Publisher :
Page : 41 pages
File Size : 12,29 MB
Release : 1970
Category : Pilot ejection seats
ISBN :
This specification covers the requirements for capsule-type emergency escape systems for use on aicraft capable of exceeding 600 knots equivalent airspeed (KEAS) or altitudes of 50,000 feet.
Special Study: Safety Aspects of Emergency Evacuations from Air Carrier Aircraft
United States. Bureau of Aviation Safety
Author : United States. Bureau of Aviation Safety
Publisher :
Page : 62 pages
File Size : 14,72 MB
Release : 1974
Category : Aircraft accidents
ISBN :
A Study of Open Seat Aircraft Emergency Escape Systems
Wallace R. Wade
Author : Wallace R. Wade
Publisher :
Page : 72 pages
File Size : 22,43 MB
Release : 1966
Category :
ISBN :
A study of open seat aircraft emergency escape systems is presented. Special attention is directed toward thrust requirements necessary to achieve improved seat trajectories. A two-dimensional, three degrees-of-freedom mathematical model of a rocket-powered ejection seat trajectory, including means of attitude stabilization, has been formulated. This resulting mathematical model has been programmed on both a digital computer and an analog computer. On the basis of available aerodynamic and trajectory data, a representative ejection seat configuration was selected for study. Typical trajectories were computed using the mathematical model. Parametric studies directed toward providing a guide for achieving improved escape trajectories were conducted and summarizing graphs are presented. These parameters include aircraft velocity, aircraft pitch angle, main rocket size, vernier rocket thrust, and thrust misalignment.