FIELD: aviation. SUBSTANCE: crew cabin 4 in the flight vehicle can be ejected, it is located in fin 2 of the flight vehicle, and hatch door 15 of the cargo compartment is located in the nose section of fuselage 1. Crew cabin 4 is provided with a parachute system. TV camera 10 can be located of the fuselage nose section (on hatch door 5). EFFECT: improved service properties and enhanced safety of crew. 4 dwg
Title | Year | Author | Number |
---|---|---|---|
AIRCRAFT | 1992 |
|
RU2028966C1 |
AIRCRAFT | 1992 |
|
RU2026239C1 |
AIRCRAFT | 0 |
|
SU1819800A1 |
AIRCRAFT | 1996 |
|
RU2120394C1 |
AMPHIBIOUS WITH INCREASED CARRYING CAPACITY | 2020 |
|
RU2739451C1 |
FLYING VEHICLE | 0 |
|
SU1827363A1 |
AMPHIBIA | 1999 |
|
RU2174080C2 |
AIRCRAFT | 2000 |
|
RU2176209C1 |
AIRCRAFT | 2009 |
|
RU2407672C1 |
HELICOPTER | 1992 |
|
RU2009078C1 |
Authors
Dates
1995-01-27—Published
1992-09-30—Filed