Mi G-8

GPTKB entity

Statements (57)
Predicate Object
gptkbp:instance_of gptkb:aircraft
gptkbp:bfsLayer 6
gptkbp:bfsParent gptkb:Mi_G-9
gptkbp:aircraft_operated gptkb:aircraft
gptkb:Mikhail_Gurevich
gptkb:Mi_G-15
conventional
low-wing
125 kg/m²
gptkbp:armament gptkb:none
gptkbp:climb_rate 10 m/s
gptkbp:cockpit tandem seating
gptkbp:crew 2
gptkbp:date 1946
gptkbp:decommissioned gptkb:1955
gptkbp:design gptkb:Mikoyan_and_Gurevich
training and liaison
gptkbp:engine gptkb:M-11
gptkbp:engine_type turbofan
gptkbp:features high aspect ratio wings
gptkbp:first_flight gptkb:1955
1947
gptkbp:fuel_capacity 600 L
gptkbp:height 3.1 m
https://www.w3.org/2000/01/rdf-schema#label Mi G-8
gptkbp:influenced_by Mi G-15 design
gptkbp:introduced 1948
gptkbp:landing_gear tricycle gear
gptkbp:length 8.5 m
gptkbp:manufacturer gptkb:Mikoyan
gptkbp:material gptkb:item
gptkbp:max_speed 600 km/h
gptkbp:max_takeoff_weight 3,000 kg
2,500 kg
gptkbp:nickname gptkb:Rook
gptkbp:number_built approximately 100
gptkbp:operational_area training missions
gptkbp:operational_history used in training and evaluation
gptkbp:origin gptkb:Monarch
gptkbp:primary_user gptkb:Soviet_Air_Force
gptkbp:production_years 1947-1950
gptkbp:propulsion gptkb:engine
0.5
gptkbp:range 1,200 km
gptkbp:retired 1950s
gptkbp:role gptkb:aircraft
gptkbp:roll_rate 5°/s
gptkbp:service_ceiling 10,000 m
gptkbp:services 1948
1948-1955
gptkbp:speed 120 km/h
gptkbp:successor gptkb:Mi_G-15
gptkbp:type gptkb:aircraft
gptkbp:variant gptkb:Mi_G-8_U
gptkbp:weight 1,800 kg
gptkbp:wing_area 20 m²
gptkbp:wingspan 10.5 m