Aestrup-Sibrian MRCA: Difference between revisions
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|type = {{wpl|Multirole combat aircraft}} | |type = {{wpl|Multirole combat aircraft}} | ||
|national origin = {{flag|Acrea}} <br> {{flag|Ruvelka}} | |national origin = {{flag|Acrea}} <br> {{flag|Ruvelka}} | ||
|manufacturer = Aestrup Luftfahrtsselskab AB (until | |manufacturer = Aestrup Luftfahrtsselskab AB (until 1980) <br> [[Mattson-Dyrssen-Aestrup|Mattson-Dyrssen-Aestrup Luftraumsystemet AB]] (after 1980) <br> Sibrian Aeronautics | ||
|design group = | |design group = | ||
|designer = | |designer = | ||
|builder = | |builder = | ||
|first flight = 10 May | |first flight = 10 May 1968 | ||
|introduction = | |introduction = | ||
|introduced = 13 July | |introduced = 13 July 1974 | ||
|retired = | |retired = | ||
|status = | |status = | ||
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* '''Wing Area:''' 46 m2 (500 sq ft) | * '''Wing Area:''' 46 m2 (500 sq ft) | ||
* '''Empty Weight:''' 9,500 kg (20,944 lb) | * '''Empty Weight:''' 9,500 kg (20,944 lb) | ||
* '''Powerplant:''' 1 x MDA EJ- | * '''Powerplant:''' 1 x MDA EJ-752 afterburning turbofan, 83.6 kN (18,800 lbf) thrust dry, 115.49 kN (25,738 lbf) reheat | ||
===Performance=== | ===Performance=== | ||
* '''Maximum Speed:''' Mach | * '''Maximum Speed:''' Mach 1.8 at altitude | ||
* '''Service Ceiling:''' 18,000 m (59,000 ft) | * '''Service Ceiling:''' 18,000 m (59,000 ft) | ||
Revision as of 03:17, 1 September 2021
Aestrup-Sibrian MRCA | |
---|---|
Role | Multirole combat aircraft |
National origin | Acrea Ruvelka |
Manufacturer | Aestrup Luftfahrtsselskab AB (until 1980) Mattson-Dyrssen-Aestrup Luftraumsystemet AB (after 1980) Sibrian Aeronautics |
First flight | 10 May 1968 |
Introduction | 13 July 1974 |
Primary user | Royal Acrean Air Force Ruvelkan Imperial Air Force |
The Aestrup-Sibrian MRCA is a series of single-engine, delta-wing fighters designed by Aestrup Luftfahrtsselskab AB of Acrea and Sibrian Aeronautics of Ruvelka for the Acrean Air Force and the Ruvelkan Imperial Air Force.
Development
Design
Operational History
Variants
Operators
Operators
Specifications (EF-131A Block 71)
General Characteristics
- Crew: 1
- Length: 16.4 m (53 ft 10 in)
- Wingspan: 10.6 m (34 ft 9 in)
- Height: 5.9 m (19 ft 4 in)
- Wing Area: 46 m2 (500 sq ft)
- Empty Weight: 9,500 kg (20,944 lb)
- Powerplant: 1 x MDA EJ-752 afterburning turbofan, 83.6 kN (18,800 lbf) thrust dry, 115.49 kN (25,738 lbf) reheat
Performance
- Maximum Speed: Mach 1.8 at altitude
- Service Ceiling: 18,000 m (59,000 ft)
Armament
- Guns: 1 x 20mm revolver cannon with 640 rounds
- Payload: 8 hardpoints for ordnance
See Also
- Aircraft of Comparable Role, Configuration, and Era