ASA VOT 14 Hotvemm (Pacifica): Difference between revisions
No edit summary |
|||
(21 intermediate revisions by the same user not shown) | |||
Line 1: | Line 1: | ||
{|{{Infobox aircraft begin | |||
| name = ASA VOT 14 Hotvemm | |||
| image = Q9fIMvH.png | |||
| caption = Two [[Sedunnic Air Force (Pacifica)|Sedunnic Air Force]] VOT 14 As | |||
| alt = | |||
}}{{Infobox aircraft type | |||
| type = [[Wiki:Multirole combat aircraft|Multirole fighter]] | |||
| national origin = [[Sedunn (Pacifica)|Sedunn]] | |||
| manufacturer = [[List of companies of Sedunn (Pacifica)|ASA]] | |||
| first flight = {{Start date and age|2006|09|13|df=yes}} (VOT 14 A) | |||
| introduced = {{ubl|VOT 14 A: 2 March 2014|VOT 14 S: 28 November 2016}} | |||
| status = In service | |||
| primary user = [[Sedunnic Air Force (Pacifica)|Sedunnic Air Force]] | |||
| more users = {{ubl|[[Sedunnic Navy (Pacifica)|Sedunnic Navy]]|Erinoran Air Force|Frost Army|See [[#Operators|''Operators'' section]] for others}}<!-- Limit is three (3) users in 'more users' field, four (4) total users. --> | |||
| produced = 2006–present | |||
| number built = 500+ | |||
| developed from = | |||
| variants with their own articles = | |||
| developed into = | |||
}} | |||
|} | |||
Though having some key stealth features that reduce the radar cross-section, the Hotvemm is not considered a full stealth aircraft. The design chosen is a cost-reducing compromise, but is also uncertain how effective stealth design will be against modern and future radar and missile systems. | The '''ASA VOT 14 Hotvemm''' (<small>IPA:</small> [<nowiki/>[[Sedunnic language (Pacifica)#Phonology|ˈhuːtvemː]]]; Austral: ''shadow'') is a single-engine, canard delta-wing, [[Wikipedia:Stealth|stealth]] [[Wikipedia:Multirole combat aircraft|multirole fighter]] aircraft designed and built by [[List of companies of Sedunn (Pacifica)|ASA]] by request of the Sedunnic Military Materiel Agency for use in the [[Sedunnic Air Force (Pacifica)|Sedunnic Air Force]] and the [[Sedunnic Navy (Pacifica)|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 [[Sedunnic Air Force#Doctrine|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 (Pacifica)|Erinor & Sereva]] and the [[Frost Empire (Pacifica)|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 == | |||
During the 1980s and 1990s several pre-studies had been conducted by the Sedunnic Materiel Procurement Agency and ASA that resulted in the LOHI program that was to develop a unified replacement multirole fighter for the Sedunnic Air Force's ASA VO 82 and ASA T73 and Navy's ASA S 74. Requirements included affordability, low signatures (stealth), good short-field performance to be usable within the classical Sedunnic force dispersal doctrine and on aircraft carriers, fast turnaround (mission preparations) and ability to work within highly contested airspace. This combination of requirements was considered too unique to find suitable foreign fighters for procurement. | |||
== 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 [[Wikipedia:Canard (aeronautics)|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 [[Wikipedia:Relaxed stability#Intentional instability|intentional instability]], enabled by digital fly-by-wire control system. | |||
=== Sensors and avionics === | |||
=== Stealth and signatures === | |||
=== Engine === | |||
=== Cockpit === | |||
=== Armaments and equipment === | |||
=== Availability and maintenance === | |||
The VOT 14 is notable for its minimised maintenance needs and fast turnaround time. The aircraft can land on 600-m long roads, receive basic maintenance, refuel and reload and take off in as fast as ten minutes depending on mission. An onboard monitoring system monitors the performance of the aircraft and its systems. The modular design of the VOT 14 enables frequent updates of hardware and software. | |||
=== Variants === | |||
== Operational history == | |||
== Notable accidents == | |||
== Variants == | |||
'''VOT 14 A''' | |||
The VOT 14 A is the standard variant and exists in the greatest numbers. | |||
'''VOT 14 B''' | |||
The VOT 14 B is a twin-seat variant for training, specialised attack missions and type conversion. Compared to the A-version, the airframe has been lengthened 0.75 m and the revolver cannon has been removed. | |||
'''VOT 14 S''' | |||
The F-35C is a carrier-based variant of the A-version. It has a strengthened airframe and adapted landing gear to allow for [[Wikipedia:CATOBAR|catapult-assisted take-off, barrier arrested recovery]] operations. | |||
== Operators == | |||
As of 2022 there were 462 VOT 14s in service. | |||
; {{flag|Erinor & Sereva}} | |||
* Erinoran Air Force – 36 VOT 14 As operational as of 2022 | |||
; {{flag|Frost Empire}} | |||
* Frost Army – unknown amount on order as of 2022 | |||
; {{flag|Sedunn}} | |||
* [[Sedunnic Air Force (Pacifica)|Sedunnic Air Force]] – 340 VOT 14 As and Bs as of 2022 | |||
* [[Sedunnic Navy (Pacifica)|Sedunnic Navy]] – 126 VOT 14 Ss operational as of 2022 | |||
== Specifications (VOT 14 A) == | |||
{{Aircraft specs | |||
|ref=<!-- reference --> | |||
|prime units?=met <!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, | |||
met(ric) first for all others. You MUST choose a format, or no specifications will show --> | |||
<!-- | |||
General characteristics | |||
--> | |||
|genhide= | |||
|crew=1 | |||
|capacity= | |||
|length m=16.7 | |||
|length ft= | |||
|length in= | |||
|span m=10.2 | |||
|span ft= | |||
|span in= | |||
|swept m=<!-- swing-wings --> | |||
|swept ft=<!-- swing-wings --> | |||
|swept in=<!-- swing-wings --> | |||
|height m= | |||
|height ft= | |||
|height in= | |||
|wing area sqm=47 | |||
|wing area sqft= | |||
|wing area note= | |||
|swept area sqm=<!-- swing-wings --> | |||
|swept area sqft=<!-- swing-wings --> | |||
|aspect ratio=<!-- sailplanes --> | |||
|airfoil= | |||
|empty weight kg=10000 | |||
|empty weight lb= | |||
|empty weight note= | |||
|gross weight kg=15300 | |||
|gross weight lb= | |||
|gross weight note= | |||
|max takeoff weight kg=23000 | |||
|fuel capacity=6,200 kg internal (13,670 lb) | |||
|more general= | |||
<!-- | |||
Powerplant | |||
--> | |||
|eng1 number= 1 | |||
|eng1 name= Gestallu UT-14 | |||
|eng1 type= [[Wikipedia:Afterburner|afterburning]] [[Wikipedia:Turbofan|turbofan]] | |||
|eng1 kw=<!-- prop engines --> | |||
|eng1 hp=<!-- prop engines --> | |||
|eng1 shp=<!-- prop engines --> | |||
|eng1 kn= 110<!-- jet/rocket engines --> | |||
|eng1 lbf=<!-- jet/rocket engines --> | |||
|power original= | |||
|thrust original= | |||
|eng1 kn-ab=170 <!-- afterburners --> | |||
|eng1 lbf-ab=<!-- afterburners --> | |||
|more power= | |||
|prop blade number=<!-- propeller aircraft --> | |||
|prop name= | |||
|prop dia m=<!-- propeller aircraft --> | |||
|prop dia ft=<!-- propeller aircraft --> | |||
|prop dia in=<!-- propeller aircraft --> | |||
|prop note= | |||
<!-- | |||
Performance | |||
--> | |||
|perfhide= | |||
|max speed kmh= | |||
|max speed mph= | |||
|max speed kts= | |||
|max speed mach= 1.8 at altitude<!-- supersonic aircraft --> | |||
|cruise speed kmh=<!-- if max speed unknown --> | |||
|cruise speed mph=<!-- if max speed unknown --> | |||
|cruise speed kts= | |||
|never exceed speed kmh= | |||
|never exceed speed mph= | |||
|never exceed speed kts= | |||
|range km= 2200 | |||
|range miles= | |||
|range nmi= | |||
|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 nmi= | |||
|endurance=<!-- if range unknown --> | |||
|ceiling m=16000 | |||
|ceiling ft= | |||
|g limits=+9/-3 <!-- aerobatic --> | |||
|roll rate=<!-- aerobatic --> | |||
|climb rate ms= | |||
|climb rate ftmin= | |||
|lift to drag= | |||
|wing loading kg/m2= | |||
|wing loading lb/sqft= | |||
|wing loading note= | |||
|thrust/weight=1.13 at gross weight (0.75 at maximum takeoff weight) | |||
|more performance= | |||
<!-- | |||
Armament | |||
--> | |||
<!--|armament= add bulletted list here or if you want to use the following | |||
specific parameters, remove this parameter--> | |||
|guns= 1 × 25 mm calibre HJJ 1D revolver cannon, 160 rounds | |||
|bombs= | |||
|rockets= | |||
|missiles= | |||
|hardpoints= 3 × internal stations, 6 × external stations on wings, 1 × external station under fuselage | |||
|hardpoint capacity= {{convert|1700|kg}} internal, {{convert|6200|kg}} external, {{convert|7900|kg}} total weapons payload | |||
|hardpoint rockets= | |||
|hardpoint missiles=<br> | |||
*** [[Wikipedia:Air-to-air missile|Air-to-air missiles]]: | |||
**** LAK 2 infrared short-range air-to-air missile | |||
**** LAK 4 infrared short-range air-to-air missile | |||
**** LAK 5 R active transmit-receive radar medium-range air-to-air missile | |||
**** ILO 74 Taks active radar [[Wikipedia:Ramjet|ramjet]] medium-range air-to-air missile | |||
*** [[Wikipedia:Air-to-surface missile|Air-to-surface missiles]]: | |||
**** DEM ASK air-launched cruise missile | |||
**** Vigo T5-4 anti-ship missile | |||
**** HUHH 14 anti-radiation missile | |||
**** DEM RE 3 loitering cruise missile | |||
**** MIN 22 KLIG air-to-surface missile | |||
**** Tevv 4 nuclear cruise missile | |||
|hardpoint bombs=<br> | |||
**** S55 G laser-guided bomb | |||
**** S78 D satellite positioning bomb | |||
**** YTR 444 precision glide bomb | |||
**** YTR G-8 small-diameter glide bomb | |||
|hardpoint other=external fuel tanks, targetting, reconnaissance and electronic countermeasures pods | |||
|avionics= | |||
* SLU EEG 5T [[Wikipedia:AESA|AESA]] radar | |||
* SLU MARVEN 5-9 speherical [[Wikipedia:Electro-optical targeting system|electro-optical targeting and detection system]] | |||
* SLU/VIS FEJ-H electronic warfare system | |||
}} | |||
<!--Though having some key stealth features that reduce the radar cross-section, the Hotvemm is not considered a full stealth aircraft. The design chosen is a cost-reducing compromise, but is also uncertain how effective stealth design will be against modern and future radar and missile systems. | |||
There are three variants of the Hotvemm: | There are three variants of the Hotvemm: | ||
Line 20: | Line 227: | ||
*Combat radius: | *Combat radius: | ||
**Air-to-ground: 1,500 km (internal + maximum external fuel) | **Air-to-ground: 1,500 km (internal + maximum external fuel) | ||
**Combat air patrol: 900 km (internal + maximum external fuel) | **Combat air patrol: 900 km (internal + maximum external fuel)--> | ||
[[category:Sedunn (Pacifica)]] | [[category:Sedunn (Pacifica)]] | ||
[[category:Military of Sedunn (Pacifica)]] | [[category:Military of Sedunn (Pacifica)]] |
Latest revision as of 22:27, 2 March 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
During the 1980s and 1990s several pre-studies had been conducted by the Sedunnic Materiel Procurement Agency and ASA that resulted in the LOHI program that was to develop a unified replacement multirole fighter for the Sedunnic Air Force's ASA VO 82 and ASA T73 and Navy's ASA S 74. Requirements included affordability, low signatures (stealth), good short-field performance to be usable within the classical Sedunnic force dispersal doctrine and on aircraft carriers, fast turnaround (mission preparations) and ability to work within highly contested airspace. This combination of requirements was considered too unique to find suitable foreign fighters for procurement.
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
Availability and maintenance
The VOT 14 is notable for its minimised maintenance needs and fast turnaround time. The aircraft can land on 600-m long roads, receive basic maintenance, refuel and reload and take off in as fast as ten minutes depending on mission. An onboard monitoring system monitors the performance of the aircraft and its systems. The modular design of the VOT 14 enables frequent updates of hardware and software.
Variants
Operational history
Notable accidents
Variants
VOT 14 A The VOT 14 A is the standard variant and exists in the greatest numbers.
VOT 14 B The VOT 14 B is a twin-seat variant for training, specialised attack missions and type conversion. Compared to the A-version, the airframe has been lengthened 0.75 m and the revolver cannon has been removed.
VOT 14 S The F-35C is a carrier-based variant of the A-version. It has a strengthened airframe and adapted landing gear to allow for catapult-assisted take-off, barrier arrested recovery operations.
Operators
As of 2022 there were 462 VOT 14s in service.
- Erinoran Air Force – 36 VOT 14 As operational as of 2022
- Frost Army – unknown amount on order as of 2022
- Sedunnic Air Force – 340 VOT 14 As and Bs as of 2022
- Sedunnic Navy – 126 VOT 14 Ss operational as of 2022
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/-3
- Thrust/weight: 1.13 at gross weight (0.75 at maximum takeoff weight)
Armament
- Guns: 1 × 25 mm calibre HJJ 1D revolver cannon, 160 rounds
- Hardpoints: 3 × internal stations, 6 × external stations on wings, 1 × external station under fuselage with a capacity of 1,700 kilograms (3,700 lb) internal, 6,200 kilograms (13,700 lb) external, 7,900 kilograms (17,400 lb) total weapons payload,with provisions to carry combinations of:
- Missiles:
- Air-to-air missiles:
- LAK 2 infrared short-range air-to-air missile
- LAK 4 infrared short-range air-to-air missile
- LAK 5 R active transmit-receive radar medium-range air-to-air missile
- ILO 74 Taks active radar ramjet medium-range air-to-air missile
- Air-to-surface missiles:
- DEM ASK air-launched cruise missile
- Vigo T5-4 anti-ship missile
- HUHH 14 anti-radiation missile
- DEM RE 3 loitering cruise missile
- MIN 22 KLIG air-to-surface missile
- Tevv 4 nuclear cruise missile
- Air-to-air missiles:
- Bombs:
- S55 G laser-guided bomb
- S78 D satellite positioning bomb
- YTR 444 precision glide bomb
- YTR G-8 small-diameter glide bomb
- Other: external fuel tanks, targetting, reconnaissance and electronic countermeasures pods
- Missiles:
Avionics
- SLU EEG 5T AESA radar
- SLU MARVEN 5-9 speherical electro-optical targeting and detection system
- SLU/VIS FEJ-H electronic warfare system