ASA VOT 14 Hotvemm (Pacifica): Difference between revisions
(→Design) Tag: 2017 source edit |
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|eng1 hp=<!-- prop engines --> | |eng1 hp=<!-- prop engines --> | ||
|eng1 shp=<!-- prop engines --> | |eng1 shp=<!-- prop engines --> | ||
|eng1 kn=<!-- jet/rocket engines --> | |eng1 kn= 110<!-- 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=170 <!-- afterburners --> | ||
|eng1 lbf-ab=<!-- afterburners --> | |eng1 lbf-ab=<!-- afterburners --> | ||
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|max speed mph= | |max speed mph= | ||
|max speed kts= | |max speed kts= | ||
|max speed mach=<!-- supersonic aircraft --> | |max speed mach= 1.8 at altitude<!-- supersonic aircraft --> | ||
|cruise speed kmh=<!-- if max speed unknown --> | |cruise speed kmh=<!-- if max speed unknown --> | ||
|cruise speed mph=<!-- if max speed unknown --> | |cruise speed mph=<!-- if max speed unknown --> | ||
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|never exceed speed mph= | |never exceed speed mph= | ||
|never exceed speed kts= | |never exceed speed kts= | ||
|range km= | |range km= 2200 | ||
|range miles= | |range miles= | ||
|range nmi= | |range nmi= | ||
|combat range km= | |combat range km= 1000 | ||
|combat range note=interdiction mission (air-to-surface) on internal fuel | |||
** {{cvt|1100|km|mi nmi}}, air-to-air configuration on internal fuel | |||
|combat range miles= | |combat range miles= | ||
|combat range nmi= | |combat range nmi= | ||
|endurance=<!-- if range unknown --> | |endurance=<!-- if range unknown --> | ||
|ceiling m= | |ceiling m=16000 | ||
|ceiling ft= | |ceiling ft= | ||
|g limits=<!-- aerobatic --> | |g limits=+9 <!-- aerobatic --> | ||
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|wing loading lb/sqft= | |wing loading lb/sqft= | ||
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|thrust/weight=1.13 at gross weight (0.75 at maximum takeoff weight) | |||
|more performance= | |more performance= | ||
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Revision as of 23:58, 17 February 2024
| ASA VOT 14 Hotvemm | |
|---|---|
| |
| Two Sedunnic Air Force VOT 14 As | |
| Role | Multirole fighter |
| National origin | Sedunn |
| Manufacturer | ASA |
| First flight | 13 September 2006 (VOT 14 A) |
| Introduction |
|
| Status | In service |
| Primary users | Sedunnic Air Force
|
| Produced | 2006–present |
| Number built | 500+ |
The ASA VOT 14 Hotvemm (IPA: [ˈhuːtvemː]; Austral: shadow) is a single-engine, canard delta-wing, stealth multirole fighter aircraft designed and built by ASA by request of the Sedunnic Military Materiel Agency for use in the Sedunnic Air Force and the Sedunnic Navy. The VOT 14 is capable of shifting between air supremacy, interdiction, reconnaissance and attack roles during flight and is thus also labelled a swing-role fighter. The VOT 14 is capable of aerial refuelling and is designed to allow landing on rudimentary runways and public roads as part of the Sedunnic force dispersal doctrine. Variants exist that have two seats (VOT 14 B) or are carrier-based (VOT 14 S). As of 2022, over 500 VOT 14s have been built.
The VOT 14's first flight occurred in in 2006 and the first aircraft entered service with the Sedunnic Air Force in March 2014 and the Sedunnic Navy in November 2016. The aircraft has been exported to Erinor & Sereva and the Frost Empire. The aircraft first saw limited action in the later phase of the Military Intervention Against Soormann in 2015 and full-scale combat in 2018 during the Reizen Civil War (Pacifica).
Development
Design
The VOT 14 is a single-engine, supersonic, stealth multirole fighter. Its design emphasises good short take-off and landing performance, low maintenance requirements, modularity and long range lethality. The aircraft has canard control surfaces that generate positive lift at all speeds, and has a delta wing that compensates for the negative lift produced by the pair of rear stabilisers. The canards and rear stabilisers angle downwards to act as air brakes to decrease the landing distance. The airframe is strengthened to withstand a high sink rate. High manoeuvrability is achieved through intentional instability, enabled by digital fly-by-wire control system.
Sensors and avionics
Stealth and signatures
Engine
Cockpit
Armaments and equipment
Maintenance
Variants
Operational history
Notable accidents
Variants
Operators
Specifications (VOT 14 A)
General characteristics
- Crew: 1
- Length: 16.7 m (54 ft 9 in)
- Wingspan: 10.2 m (33 ft 6 in)
- Wing area: 47 m2 (510 sq ft)
- Empty weight: 10,000 kg (22,046 lb)
- Gross weight: 15,300 kg (33,731 lb)
- Max takeoff weight: 23,000 kg (50,706 lb)
- Fuel capacity: 6,200 kg internal (13,670 lb)
- Powerplant: 1 × Gestallu UT-14 afterburning turbofan, 110 kN (25,000 lbf) thrust dry, 170 kN (38,000 lbf) with afterburner
Performance
- Maximum speed: Mach 1.8 at altitude
- Range: 2,200 km (1,400 mi, 1,200 nmi)
- Combat range: 1,000 km (620 mi, 540 nmi) interdiction mission (air-to-surface) on internal fuel
- 1,100 km (680 mi; 590 nmi), air-to-air configuration on internal fuel
- Service ceiling: 16,000 m (52,000 ft)
- g limits: +9
- Thrust/weight: 1.13 at gross weight (0.75 at maximum takeoff weight)