Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:archaeological_site
|
| gptkbp:bfsLayer |
6
|
| gptkbp:bfsParent |
gptkb:Martin-Baker_Mk._15
|
| gptkbp:deployment |
rocket-assisted ejection
|
| gptkbp:developer |
based on earlier models
|
| gptkbp:elevation |
up to 50,000 feet
|
| gptkbp:features |
zero-zero capability
|
| gptkbp:historical_significance |
widely used in the 1960s and 1970s
|
| https://www.w3.org/2000/01/rdf-schema#label |
Martin-Baker Mk. 39
|
| gptkbp:introduced |
1960s
|
| gptkbp:is_compatible_with |
various aircraft types
|
| gptkbp:is_designed_for |
high-speed aircraft
|
| gptkbp:manufacturer |
gptkb:Martin-Baker_Aircraft_Company
|
| gptkbp:max_takeoff_weight |
automatic or manual
up to 600 knots |
| gptkbp:notable_users |
British military
|
| gptkbp:operational_area |
gptkb:military_base
|
| gptkbp:safety_record |
high safety record
|
| gptkbp:seating_capacity |
catapult seat
|
| gptkbp:succeeded_by |
over 90%
|
| gptkbp:successor |
gptkb:Martin-Baker_Mk._40
|
| gptkbp:type |
gptkb:archaeological_site
|
| gptkbp:used_in |
gptkb:aircraft
|
| gptkbp:weight |
approximately 100 kg
|