Accession Number:

AD0871324

Title:

Study and Design of an Ejection System for VTOL Aircraft. Part 2. Volume 1. Escape Seat System Concept Analysis.

Descriptive Note:

Final rept. Apr 69-Apr 70,

Corporate Author:

LTV AEROSPACE CORP DALLAS TX VOUGHT AERONAUTICS DIV

Personal Author(s):

• Cartwright, E. O., Jr.
• Clinkenbeard, I. L.

Report Date:

1970-06-01

Pagination or Media Count:

302.0

Abstract:

Descriptors:

• *JETTISONABLE COCKPITS
• *VERTICAL TAKEOFF AIRCRAFT
• *JET FIGHTERS
• AEROSPACE SYSTEMS
• LOW ALTITUDE
• REDUNDANT COMPONENTS
• DROGUE PARACHUTES
• OPERATION
• VERNIER ROCKET ENGINES
• ROCKET PROPULSION
• RECOVERY
• RELIABILITY
• RELIABILITY

Subject Categories:

• Gliders and Parachutes
• Escape, Rescue and Survival

Distribution Statement:

APPROVED FOR PUBLIC RELEASE