Reference to experimental work and developments by Martin Baker Aircraft Co since 1944; present Mark III seat carries out whole ejection and descent assuming pilot to be unconscious after operating face blind; it is similar to Mark I, but incorporates timing mechanism with barostat valve; device releases drogue shackle after delay of 4 sec provided seat is below 10,000 ft altitude; illustrations. (See also Engineer v 190 n 4951 Dec 15 1950 p 599-600)
Escape equipment on high speed aircraft
Engineering
Engineering ; 171 , n 4444
1951
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Escape equipment on high speed aircraft
Engineering Index Backfile | 1950
Escape from high-speed aircraft
Engineering Index Backfile | 1955
|Emergency escape equipment for high-speed rail train and use method of emergency escape equipment
European Patent Office | 2022
|Escape from High Performance Aircraft
NTIS | 1956
|Escape from high-performance aircraft
Engineering Index Backfile | 1957
|