gptkbp:instance_of
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gptkb:furniture
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gptkbp:canopy_separation
|
pyrotechnic system
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gptkbp:control_system
|
manual and automatic
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gptkbp:crew_capacity
|
gptkb:1
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gptkbp:deployment
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gptkb:People's_Liberation_Army_Air_Force
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gptkbp:design_purpose
|
pilot safety
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gptkbp:designed_by
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gptkb:Shenyang_Aircraft_Corporation
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gptkbp:development
|
1990s
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gptkbp:elevation
|
up to 15,000 meters
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gptkbp:emergency_services
|
in case of aircraft malfunction
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gptkbp:ergonomics
|
pilot-friendly design
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gptkbp:exported_to
|
no known exports
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gptkbp:features
|
rocket-assisted ejection
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gptkbp:first_flight
|
gptkb:2006
|
https://www.w3.org/2000/01/rdf-schema#label
|
WS-10 ejection seat
|
gptkbp:influenced_by
|
Western ejection seat designs
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gptkbp:introduced_in
|
2000s
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gptkbp:involved_technology
|
ejection seat technology
|
gptkbp:is_similar_to
|
gptkb:Martin-Baker_ejection_seats
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gptkbp:is_tested_for
|
completed in 2005
|
gptkbp:is_trained_in
|
five-point harness
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gptkbp:maintenance
|
routine checks required
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gptkbp:manufacturer
|
gptkb:China
|
gptkbp:material
|
lightweight alloys
|
gptkbp:modifications
|
upgrades over time
|
gptkbp:notable_case
|
successful ejections recorded
|
gptkbp:operational_history
|
in service since 2006
|
gptkbp:project
|
ongoing research for improvements
|
gptkbp:reclining_angle
|
30 degrees
|
gptkbp:related_aircraft
|
various Chinese military aircraft
|
gptkbp:related_to
|
gptkb:military_aircraft
|
gptkbp:safety_features
|
integrated parachute system
|
gptkbp:safety_rating
|
high
|
gptkbp:seat_pan
|
adjustable
|
gptkbp:speed
|
up to Mach 2.5
|
gptkbp:successor
|
WS-9 ejection seat
|
gptkbp:takeoff_distance
|
controlled by pilot
catapult and gravity
|
gptkbp:training
|
provided to pilots
|
gptkbp:type
|
gptkb:zero-zero_ejection_seat
|
gptkbp:used_in
|
gptkb:Shenyang_J-11
gptkb:Shenyang_J-15
|
gptkbp:user_countries
|
gptkb:China
|
gptkbp:weight
|
approximately 100 kg
|
gptkbp:bfsParent
|
gptkb:J-15
|
gptkbp:bfsLayer
|
6
|