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gptkbp:instance_of
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gptkb:archaeological_site
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gptkbp:bfsLayer
|
6
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gptkbp:bfsParent
|
gptkb:Martin-Baker_Mk._15
|
|
gptkbp:controls
|
electromechanical
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|
gptkbp:deployment
|
manual and automatic
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|
gptkbp:developer
|
1950-1955
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|
gptkbp:elevation
|
from ground level to 50,000 feet
|
|
gptkbp:emergency_services
|
manual override system
|
|
gptkbp:features
|
rocket-assisted ejection
reclined seat position
|
|
gptkbp:feedback
|
positive reviews from pilots
|
|
gptkbp:first_introduced
|
gptkb:military_base
|
|
gptkbp:height
|
1.2 meters
|
|
gptkbp:historical_significance
|
improved pilot safety
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Martin-Baker Mk. 34
|
|
gptkbp:introduced
|
1950s
|
|
gptkbp:involved_units
|
over 1,000
|
|
gptkbp:is_designed_for
|
high-speed aircraft
|
|
gptkbp:is_tested_for
|
completed in 1956
|
|
gptkbp:legacy
|
influenced future ejection seat designs
|
|
gptkbp:manufacturer
|
gptkb:Martin-Baker_Aircraft_Company
|
|
gptkbp:max_takeoff_weight
|
up to 600 knots
|
|
gptkbp:notable_event
|
successful ejections in combat
|
|
gptkbp:notable_users
|
gptkb:British_military_aircraft
|
|
gptkbp:operational_range
|
up to 50,000 feet
|
|
gptkbp:production_years
|
gptkb:1957
gptkb:1965
|
|
gptkbp:regulatory_compliance
|
approved by military aviation authorities
|
|
gptkbp:related_model
|
gptkb:Martin-Baker_Mk._30
gptkb:Martin-Baker_Mk._32
gptkb:Martin-Baker_Mk._33
gptkb:Martin-Baker_Mk._35
|
|
gptkbp:replaced_by
|
gptkb:Martin-Baker_Mk._36
|
|
gptkbp:safety_features
|
high
|
|
gptkbp:seating_capacity
|
gptkb:zero-zero_ejection_seat
|
|
gptkbp:successor
|
gptkb:Martin-Baker_Mk._35
|
|
gptkbp:technology
|
pyrotechnic devices
ballistic recovery systems
ejection control systems
safety harness systems
seat pan design
|
|
gptkbp:training
|
pilot ejection training required
|
|
gptkbp:type
|
catapult ejection seat
|
|
gptkbp:used_in
|
gptkb:aircraft
|
|
gptkbp:weight
|
approximately 100 kg
|
|
gptkbp:width
|
0.5 meters
|