Statements (62)
Predicate | Object |
---|---|
gptkbp:instance_of |
gptkb:archaeological_site
|
gptkbp:bfsLayer |
7
|
gptkbp:bfsParent |
gptkb:Martin-Baker_Mk._21
|
gptkbp:deployment |
rocket-assisted ejection
|
gptkbp:developer |
ongoing improvements
|
gptkbp:features |
environmental protection
improved aerodynamics lightweight materials modular design reliability user-friendly interface combat readiness advanced manufacturing techniques high-performance materials cost-effectiveness sustainability considerations impact resistance customizable options streamlined design reduced weight ease of maintenance thermal protection advanced telemetry quick deployment real-time diagnostics zero-zero capability multi-role capability enhanced visibility ergonomic seating high-altitude performance modular upgrades survivability enhancements integrated parachute system future-proofing capabilities advanced safety mechanisms field repairability integration with avionics automatic activation system user training systems |
gptkbp:first_introduced |
1960s
|
gptkbp:height |
1.2 meters
|
gptkbp:historical_significance |
widely used in the 20th century
|
https://www.w3.org/2000/01/rdf-schema#label |
Martin-Baker Mk. 21 M
|
gptkbp:influenced_by |
earlier Martin-Baker models
|
gptkbp:is_designed_for |
gptkb:aircraft
|
gptkbp:manufacturer |
gptkb:Martin-Baker_Aircraft_Company
|
gptkbp:notable_users |
gptkb:Indian_Air_Force
gptkb:South_African_Air_Force gptkb:military_base gptkb:battle |
gptkbp:operational_range |
up to 50,000 feet
|
gptkbp:operational_status |
in service
|
gptkbp:regulatory_compliance |
NATO standards
|
gptkbp:related_to |
gptkb:Martin-Baker_Mk._10
|
gptkbp:replaced_by |
gptkb:Martin-Baker_Mk._22_M
|
gptkbp:safety_features |
high
|
gptkbp:successor |
gptkb:Martin-Baker_Mk._22_M
|
gptkbp:technology |
ejection seat technology
|
gptkbp:type |
catapult ejection seat
|
gptkbp:used_in |
gptkb:Hawker_Siddeley_Harrier
|
gptkbp:weight |
approximately 100 kg
|
gptkbp:width |
0.5 meters
|