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An Investigation of an Integrated Aircrew Escape/Rescue System Capability (AERCAB).


AD860590

Publication Date 1969
Personal Author Manzuk, R. J.; Peck, W. R.; Yost, C. A.; Duncan, J. W.; Braunlich, E. A.
Page Count 379
Abstract A detailed preliminary design study was accomplished, and it is shown that the system is retrofitable in the existing crew stations of the A-7 and F-4 aircraft with modifications thereto. (Author)
Keywords
  • Jet fighters
  • Ejection seats
  • Parawings
  • Aerospace systems
  • Aerodynamic characteristics
  • Air force research
  • Ejection
  • Stabilization
  • Turbofan engines
  • Parachutes
  • Navigational aids
  • Sequences(Mathematics)
  • Flight control systems
  • Maneuverability
  • Catapults
  • Hydraulic equipment
  • Homing devices
  • Safety belts
  • Survival kits
  • A-7 aircraft
  • F-4 aircraft
Source Agency
  • Non Paid Delimited ADS
NTIS Subject Category
  • 51C - Aircraft
  • 46B - Fluid Mechanics
Corporate Authors Stencel AERO Engineering Corp Asheville N C
Document Type Technical Report
Title Note Final rept. Mar-Dec 68.
NTIS Issue Number 197626
Contract Number
  • F33615-68-C-1461
An Investigation of an Integrated Aircrew Escape/Rescue System Capability (AERCAB).
An Investigation of an Integrated Aircrew Escape/Rescue System Capability (AERCAB).
AD860590

  • Jet fighters
  • Ejection seats
  • Parawings
  • Aerospace systems
  • Aerodynamic characteristics
  • Air force research
  • Ejection
  • Stabilization
  • Turbofan engines
  • Parachutes
  • Navigational aids
  • Sequences(Mathematics)
  • Flight control systems
  • Maneuverability
  • Catapults
  • Hydraulic equipment
  • Homing devices
  • Safety belts
  • Survival kits
  • A-7 aircraft
  • F-4 aircraft
  • Non Paid Delimited ADS
  • 51C - Aircraft
  • 46B - Fluid Mechanics
  • F33615-68-C-1461
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