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 | 
| FLYING VEHICLE | 0 | 
									
  | 
                SU1827363A1 | 
| AMPHIBIOUS WITH INCREASED CARRYING CAPACITY | 2020 | 
									
  | 
                RU2739451C1 | 
| AMPHIBIA | 1999 | 
									
  | 
                RU2174080C2 | 
| AIRCRAFT | 2000 | 
									
  | 
                RU2176209C1 | 
| HELICOPTER | 1992 | 
									
  | 
                RU2009078C1 | 
| AIRCRAFT | 2009 | 
									
  | 
                RU2407672C1 | 
Authors
Dates
1995-01-27—Published
1992-09-30—Filed