Statements (48)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
ejection seat
|
| gptkbp:compatibleWith |
F-16_variants
|
| gptkbp:crew_size |
up to 600 knots
|
| gptkbp:depth |
0.6 meters
|
| gptkbp:designedFor |
F-16 Fighting Falcon
high-speed ejection reduce pilot injury |
| gptkbp:developedBy |
1970s
|
| gptkbp:duration |
0.5 seconds
|
| gptkbp:features |
zero-zero capability
survival kit |
| gptkbp:has |
reclining mechanism
leg restraints |
| gptkbp:hasArea |
various flight conditions
|
| gptkbp:height |
1.2 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
Martin-Baker F-16 seat
|
| gptkbp:includes |
parachute system
seat pan |
| gptkbp:is |
ergonomically designed
lightweight durable widely used developed for military use adaptable reliable designed for high performance combat proven certified for use tested for reliability used in training aircraft integrated with safety systems a critical component of aircraft safety designed for quick ejection part of ejection seat family |
| gptkbp:is_integrated_with |
aircraft_avionics
|
| gptkbp:manufacturer |
gptkb:Martin-Baker_Aircraft_Company
|
| gptkbp:offers |
pilot harness system
|
| gptkbp:operationalStatus |
up to 50,000 feet
|
| gptkbp:provides |
pilot safety
head support |
| gptkbp:requires |
maintenance checks
|
| gptkbp:safetyFeatures |
automatic seat separation
|
| gptkbp:type |
ejection seat
|
| gptkbp:usedBy |
various air forces
|
| gptkbp:usedIn |
military aircraft
|
| gptkbp:utilizes |
pyrotechnic devices
|
| gptkbp:weight |
approximately 100 kg
|
| gptkbp:width |
0.5 meters
|