Statements (104)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
gptkb:jet_engine |
| gptkbp:aircraft_operated |
gptkb:Lockheed_A-12
|
| gptkbp:application |
gptkb:military_aircraft
|
| gptkbp:cancellation_reason |
not equipped
|
| gptkbp:certification |
FAA certified
|
| gptkbp:combustor_type |
annular
|
| gptkbp:compressor_type |
axial
|
| gptkbp:control_system |
hydromechanical
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
3 ft 4 in
3 ft 9 in |
| gptkbp:engine |
gptkb:TF30_family
gptkb:Pratt_&_Whitney_TF30 discontinued modular design scheduled maintenance advanced materials fighter jets historically significant Brayton cycle performance enhancements combat missions air start afterburner jet propulsion technology 1960s era used in multiple aircraft types |
| gptkbp:engine_configuration |
gptkb:military_law
inline twin-spool conventional design single spool high thrust output |
| gptkbp:engine_power |
high reliability
military specifications moderate efficiency combat ready phased out |
| gptkbp:engine_production_facilities |
manufacturing plants
|
| gptkbp:engine_type |
TF33-P-100 A
TF33-P-100 B TF33-P-100 C TF33-P-100 D TF33-P-100 E TF33-P-100 F TF33-P-100 G TF33-P-100 H TF33-P-100 I TF33-P-100 J TF33-P-100 K TF33-P-100 L TF33-P-100 M TF33-P-100 N TF33-P-100 O TF33-P-100 P TF33-P-100 Q TF33-P-100 R TF33-P-100 S TF33-P-100 T TF33-P-100 U TF33-P-100 V TF33-P-100 W TF33-P-100 X TF33-P-100 Y TF33-P-100 Z |
| gptkbp:first_flight |
gptkb:1960
gptkb:1964 |
| gptkbp:fuel_economy |
moderate
0.85 lb/lbf/hr |
| gptkbp:fuel_type |
gptkb:electronic
JP-4 |
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney TF33-P-100
|
| gptkbp:introduced |
gptkb:1964
|
| gptkbp:is_tested_for |
military bases
static test |
| gptkbp:length |
15 ft 9 in
13 ft 4 in |
| gptkbp:maintenance |
500 hours
1,000 hours |
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:noise_level |
high
|
| gptkbp:number_of_stages |
8
|
| gptkbp:operational_history |
used in Vietnam War
|
| gptkbp:operational_range |
high subsonic to supersonic
|
| gptkbp:propulsion |
22,000 lbf
5.79:1 6.29 |
| gptkbp:related_aircraft |
gptkb:F-111_Aardvark
F-4 Phantom II family |
| gptkbp:replaced_by |
gptkb:Pratt_&_Whitney_F119
|
| gptkbp:retired |
1990s
|
| gptkbp:service_ceiling |
50,000 ft
|
| gptkbp:service_history |
used in Vietnam War
|
| gptkbp:turbine_type |
axial
single-stage |
| gptkbp:type |
gptkb:turbofan_engine
military engine |
| gptkbp:used_in |
gptkb:Mc_Donnell_Douglas_F-4_Phantom_II
|
| gptkbp:variant |
TF33-P-100 A
|
| gptkbp:weight |
3,500 lb
3,800 lb |
| gptkbp:bfsParent |
gptkb:KC-135_Stratotanker
|
| gptkbp:bfsLayer |
4
|