Renard J/A-29 Merlet: Difference between revisions
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{{Aircraft specs | {{Aircraft specs | ||
|ref=<!-- reference --> | |ref=<!-- reference --> | ||
|prime units?= | |prime units?=met | ||
met | |||
|crew= J/A-12E: 1 (pilot), J/A-12F: 2 (pilot and {{wpl|weapon systems officer}}) | |crew= J/A-12E: 1 (pilot), J/A-12F: 2 (pilot and {{wpl|weapon systems officer}}) | ||
| Line 77: | Line 72: | ||
|length ft= | |length ft= | ||
|length in= | |length in= | ||
|span m= | |span m= | ||
|span ft= | |span ft= | ||
|span in= | |span in= | ||
|swept m=<!-- swing-wings --> | |swept m=<!-- swing-wings --> | ||
|swept ft=<!-- swing-wings --> | |swept ft=<!-- swing-wings --> | ||
|swept in=<!-- swing-wings --> | |swept in=<!-- swing-wings --> | ||
|height m= | |height m= | ||
|height ft= | |height ft= | ||
|height in= | |height in= | ||
|wing area sqm= | |wing area sqm= | ||
|wing area sqft= | |wing area sqft= | ||
| Line 115: | Line 86: | ||
|swept area sqm=<!-- swing-wings --> | |swept area sqm=<!-- swing-wings --> | ||
|swept area sqft=<!-- swing-wings --> | |swept area sqft=<!-- swing-wings --> | ||
|aspect ratio=<!-- sailplanes --> | |aspect ratio=<!-- sailplanes --> | ||
|airfoil= | |airfoil= | ||
| Line 127: | Line 94: | ||
|gross weight lb= | |gross weight lb= | ||
|gross weight note= | |gross weight note= | ||
|fuel capacity= | |fuel capacity= | ||
|more general= | |more general= | ||
<!-- | <!-- | ||
| Line 146: | Line 107: | ||
|eng1 kn=<!-- jet/rocket engines --> | |eng1 kn=<!-- jet/rocket engines --> | ||
|eng1 lbf=<!-- jet/rocket engines --> | |eng1 lbf=<!-- jet/rocket engines --> | ||
|power original= | |power original= | ||
|thrust original= | |thrust original= | ||
|eng1 kn-ab=<!-- afterburners --> | |eng1 kn-ab=<!-- afterburners --> | ||
|eng1 lbf-ab=<!-- afterburners --> | |eng1 lbf-ab=<!-- afterburners --> | ||
|more power= | |more power= | ||
| Line 182: | Line 118: | ||
|prop dia ft=<!-- propeller aircraft --> | |prop dia ft=<!-- propeller aircraft --> | ||
|prop dia in=<!-- propeller aircraft --> | |prop dia in=<!-- propeller aircraft --> | ||
|prop | |prop note= | ||
<!-- | <!-- | ||
Performance | Performance | ||
--> | --> | ||
| | |perfhide= | ||
|max speed kmh= | |||
|max speed mph= | |max speed kmh= | ||
|max speed kts= | |max speed mph= | ||
|max speed note= at 12,190 m | |max speed kts= 1,030 | ||
|cruise speed kmh= | |max speed note=at 12,190 m | ||
|cruise speed mph= | |max speed mach=1.6 | ||
|cruise speed kmh=<!-- if max speed unknown --> | |||
|cruise speed mph=<!-- if max speed unknown --> | |||
|cruise speed kts= | |cruise speed kts= | ||
| | |never exceed speed kmh= | ||
|range km= | |never exceed speed mph= | ||
|never exceed speed kts= | |||
|range km= 2,346 | |||
|range miles= | |range miles= | ||
|range nmi= | |range nmi= | ||
|combat range km= 722 | |||
|combat range km= | |||
|combat range miles= | |combat range miles= | ||
|combat range nmi= | |combat range nmi= | ||
|ferry range km= 3,330 | |||
|ferry range km= | |||
|ferry range miles= | |ferry range miles= | ||
|ferry range nmi= | |ferry range nmi= | ||
|ferry range note= | |ferry range note= | ||
|endurance=<!-- if range unknown --> | |endurance=<!-- if range unknown --> | ||
|ceiling m= | |ceiling m= 15,000 | ||
|ceiling ft= | |ceiling ft= | ||
|ceiling note= | |ceiling note= | ||
|climb rate ms= 228 | |||
|climb rate ms= | |||
|climb rate ftmin= | |climb rate ftmin= | ||
|lift to drag= | |lift to drag= | ||
|wing loading kg/m2= | |wing loading kg/m2= | ||
|wing loading lb/sqft= | |wing loading lb/sqft= | ||
|wing loading note= | |wing loading note= | ||
|power/mass= | |power/mass= | ||
|thrust/weight= | |thrust/weight= 0.93 | ||
|more performance= | |more performance=*'''Design load factor:''' 7.6 g | ||
<!-- | <!-- | ||
Armament | Armament | ||
--> | --> | ||
| | |guns= 1 x {{wpl|20 mm caliber|20mm}} ([[Fokker-Leimberger MK-47]], , 412 rounds) | ||
|bombs= | |bombs= | ||
|rockets= | |rockets= | ||
Revision as of 19:45, 27 January 2022
 | This article is incomplete because it is pending further input from participants, or it is a work-in-progress by one author. Please comment on this article's talk page to share your input, comments and questions. Note: To contribute to this article, you may need to seek help from the author(s) of this page. |
| J/A-12 Horzel | |
|---|---|
_22_approaches_for_a_touch-and-go_while_conducting_carr.jpg)
| |
| Role | Carrier-based multirole fighter |
| National origin | Rethua / Atmora |
| Manufacturer | Renard Vliegtuigfabrikant N.V. / Rethua Aerospace Systems |
| First flight | 21 August 1994 |
| Introduction | 7 March 1997 |
| Status | In service |
| Primary user | Royal Atmoran Navy Royal Mizuhese Navy |
| Produced | 1993–present |
| Number built | +916 as of September 2016 |
| Program cost | ƒ370.78 billion (NS$695.6 billion) |
| Unit cost |
ƒ37.2 million (NS$66.2 million)
|
| Developed from | MF-12 |
| Variants | Renard EJ-12 Grommelaar |
The Renard J/A-12 Horzel, 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-12Es single-seat and J/A-12Fs tandem-seat variants are larger more advanced specialised naval variants of the Rethuan RAE MF-12C/Ds fighter aircraft.
Development
Origins
Operational history
Variants
Operators
Atmoran Confederation
- Royal Atmoran Navy
- Anemoisic Fleet Squadrons
- Emporic Fleet Squadrons
- 200 Marinevliegtuigeskadron
- 204 Marinevliegtuigeskadron
- 205 Marinevliegtuigeskadron
- 244 Marinevliegtuigeskadron
- 246 Marinevliegtuigeskadron
- 257 Marinevliegtuigeskadron
- 281 Marinevliegtuigeskadron
- Test and Evaluation squadrons
- Warfighting Development Centers
- Flight Demonstration squadrons
Mizuho
Specifications (J/A-12E/F)
General characteristics
- Crew: J/A-12E: 1 (pilot), J/A-12F: 2 (pilot and weapon systems officer)
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
- Guns: 1 x 20mm (Fokker-Leimberger MK-47, , 412 rounds)