Difference between revisions of "PA-25 Multirole Fighter"
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==Variants== | ==Variants== | ||
− | [[File:Rafale Theodore Roosevelt.jpg|thumb|left|A Prizyetsi Navy PA-25 | + | [[File:Rafale Theodore Roosevelt.jpg|thumb|left|A Prizyetsi Navy PA-25 N with tail hook deployed during landing aboard an aircraft carrier.]] |
+ | *PA-25 ADF | ||
+ | *PA-25 MR | ||
+ | *PA-25 N | ||
==Specifications== | ==Specifications== |
Revision as of 17:40, 30 December 2014
The Prizyetsi Aeronotics (Prissetsä Lufteknikk) PA-25 is a multirole fighter designed by PA, a subsidiary of Sverd Industries which is the largest conglomerate in The United Federation of Prizyetsa for use by the Prizyetsi Armed Forces.
Contents
Development
Origins
Design
Overview
Powerplant
Sensors
Variants
- PA-25 ADF
- PA-25 MR
- PA-25 N
Specifications
General
- Crew: 1 or 2
- Length: 15.3m
- Wingspan: 10.8m
- Height: 5.34m
- Wing Area: 45.7m2
- Empty Weight: 9,800kg
- Loaded Weight: 14,000kg
- Max Take-off Weight: 24,500kg
- Powerplant: 2 x SJ90 Afterburning Turbofans
- Dry Thrust: 5,100kgf
- Thrust with Afterburner: 7,700kgf
- Price per Unit: NSD 30 million
Performance
- Maximum Speed: Mach 2.25 (2,400 km/h) at altitude
- Range: 2,000km
- Combat Radius: 1,000km
- Ferry Range: 3,400km (with 3 drop tanks)
- Service Ceiling: 18,000m
- Rate of Climb: 330m/s
- Thrust/Weight: 1.03
- Max. maneuvering load factor: 10,5g
Armament
- Guns: 2 x 30mm Siljeborg AC-30b autocannon (380 rounds)
- Hardpoints: 11 (6 under the wings, 5 centerline)
- Missiles
- Air to Air
- Air to Ground:
- Bombs:
- Guided and unguided bombs
Avionics
- AEPA-35 (Active Electric Phased Array)
- OTS-84 (Electro-Optical Detection System)
- RDS-G5 (Ultra-Violet Missile Approach Warning System)
Users
- Prizyetsa