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Renard J/A-29 Merlet: Difference between revisions

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|program cost  = ƒ370.78 billion (NS$695.6 billion)
|program cost  = ƒ370.78 billion (NS$695.6 billion)
|unit cost      = ƒ37.2 million (NS$66.2 million)
|unit cost      = ƒ37.2 million (NS$66.2 million)
|variants with their own articles = [[Renard EA-29G Grommelaar]]<br>[[Mitsubishi J-2 Hien Kai]]
|variants with their own articles = [[Renard EA-29G Grommelaar]]<br>[[Mitsubishi J-2 Kai]]
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Revision as of 20:41, 11 March 2022

J/A-29 Hoornaar
US Navy 111201-N-DR144-673 An F-A-18F Super Hornet assigned to Strike Fighter Squadron (VFA) 22 approaches for a touch-and-go while conducting carr.jpg
Role Carrier-based multirole fighter
National origin Atmora
Manufacturer Renard Vliegtuigfabrikant N.V.
First flight 21 August 1994
Introduction 7 March 1997
Status In service
Primary user Royal Atmoran Navy
Royal Mizuhese Navy
Royal Mizuhese Air Force
Produced 1993–present
Number built +1,916 as of September 2016
Program cost ƒ370.78 billion (NS$695.6 billion)
Unit cost
ƒ37.2 million (NS$66.2 million)
Variants Renard EA-29G Grommelaar
Mitsubishi J-2 Kai

The Renard J/A-29 Hoornaar (Hornet), are twin-engine, carrier-capable, multirole fighter aircraft is an Royal Atmoran Navy variant of the Rethuan RAE MF-12 fighter aircraft. With the Atmoran Renard J/A-29Es single-seat and J/A-29Fs tandem-seat variants are larger more advanced specialised naval variants of the Rethuan RAE MF-12C/Ds fighter aircraft.

Development

Origins

Operational history

Royal Atmoran Navy

Royal Mizuhese Navy

Variants

  • Renard J/A-29E Hoornaar: single seat variant.
  • Renard J/A-29F Hoornaar: two-seat variant.
  • Renard EA-29G Grommelaar: Electronic warfare variant of the F/A-18F

Operators

Atmora Atmoran Confederation
Mizuho Mizuho

Specifications (J/A-29E/F)

General characteristics

Performance

  • Maximum speed: 1,908 km/h; 1,185 mph (1,030 kn) at 12,190 m
  • Maximum speed: Mach 1.6
  • Range: 2,346 km (1,458 mi; 1,267 nmi)
  • Combat range: 722 km (449 mi; 390 nmi)
  • Ferry range: 3,330 km (2,069 mi; 1,798 nmi)
  • Service ceiling: 15,000 m (49,000 ft)
  • Rate of climb: 228 m/s (44,900 ft/min)
  • Thrust/weight: 0.93
  • Design load factor: 7.6 g

Armament

See also