gptkbp:instance_of
|
gptkb:rocket
|
gptkbp:aircraft_operated
|
gptkb:Mi_G-25_Foxbat
Su-22 Fitter
Mi G-31 Foxhound
Su-15 Flagon
Su-17 Fitter
|
gptkbp:controls
|
digital computer
S-75 missile system
|
gptkbp:countermeasures
|
chaff and flares
|
gptkbp:country
|
gptkb:Monarch
|
gptkbp:date
|
gptkb:1965
|
gptkbp:deployment
|
Cold War era
air bases
|
gptkbp:design
|
intercepting enemy aircraft
|
gptkbp:developer
|
1950s to 1960s
|
gptkbp:diameter
|
0.38 m
0.38 meters
|
gptkbp:elevation
|
20,000 meters
|
gptkbp:enemy
|
100 kg
150 kg
high explosive
|
gptkbp:engine_type
|
gptkb:engine
|
gptkbp:exported_to
|
gptkb:India
gptkb:Politician
gptkb:Libya
gptkb:historical_figure
some Eastern Bloc countries
|
gptkbp:features
|
large size and weight
|
gptkbp:fighting_style
|
limited
air superiority missions
|
gptkbp:first_flight
|
gptkb:1964
gptkb:1967
|
gptkbp:guidance_system
|
gptkb:hospital
high
10 seconds
active radar homing
semi-active radar homing
within 5 meters
|
gptkbp:has_programs
|
Soviet missile program
|
https://www.w3.org/2000/01/rdf-schema#label
|
R-40 missile
|
gptkbp:influence
|
subsequent missile designs
|
gptkbp:introduced
|
gptkb:1970
1960s
|
gptkbp:is_aimed_at
|
gptkb:aircraft
radar targeting
|
gptkbp:is_used_by
|
gptkb:Monarch
|
gptkbp:launch_site
|
gptkb:Mi_G-25
gptkb:Mi_G-31
|
gptkbp:launched
|
up to 45 degrees
rail launcher
|
gptkbp:length
|
gptkb:TNT
4.5 m
3.8 meters
4.1 m
|
gptkbp:manufacturer
|
gptkb:Moscow_Machine-Building_Plant
gptkb:Mikoyan
|
gptkbp:material
|
aluminum alloy
|
gptkbp:max_takeoff_weight
|
350 kg
700 kg
|
gptkbp:modifications
|
R-40 R and R-40 T variants
|
gptkbp:notable_battle
|
limited use in conflicts
|
gptkbp:notable_event
|
none documented
|
gptkbp:operational_area
|
air superiority
limited engagement scenarios
|
gptkbp:operational_range
|
100 km
50 km
|
gptkbp:operational_status
|
obsolete
|
gptkbp:produced_by
|
obsolete
|
gptkbp:propulsion
|
solid rocket motor
solid fuel
|
gptkbp:provides_information_on
|
semi-active radar homing
|
gptkbp:radar
|
N-001 radar
|
gptkbp:range
|
1 km
80 km
up to 80 km
|
gptkbp:replaced_by
|
gptkb:R-77_missile
|
gptkbp:retired
|
gptkb:Russian_Air_Force
1990s
|
gptkbp:retirement_year
|
1990s
|
gptkbp:service_ceiling
|
20,000 m
|
gptkbp:services
|
gptkb:Soviet_Air_Forces
1970s
|
gptkbp:speed
|
Mach 3.5
|
gptkbp:stealth_features
|
gptkb:none
limited
|
gptkbp:steering
|
aerodynamic control
|
gptkbp:successor
|
gptkb:R-77_missile
|
gptkbp:surface
|
four fins
|
gptkbp:targets
|
gptkb:aircraft
up to 2,500 km/h
|
gptkbp:variant
|
R-40 R
R-40 T
|
gptkbp:weight
|
600 kg
300 kg
|
gptkbp:wingspan
|
2.5 m
1.5 meters
|
gptkbp:bfsParent
|
gptkb:Vympel_Design_Bureau
|
gptkbp:bfsLayer
|
6
|