R-40 missile

GPTKB entity

Statements (98)
Predicate Object
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