Mondego (missile): Difference between revisions

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| titlestyle  = margin:0;background-color:#66023c;font-size:120%;font-weight:bold;border:1px solid #FFD700;text-align:center;color:#fff;padding:0.2em 0.4em;
| title        = '''''{{PAGENAME}}'''''
| title        = '''''{{PAGENAME}}'''''
| image        = [[File:Geneva2Launch.jpg|200px]]
| image        = [[File:Mondego-Missile-JAV.png|200px]]
| caption      = Geneva 2 Missile, launched during [[Operation Paramount]] ({[AN|1698}})
| caption      = Mondego 2 Missile, {{AN|1698}}
| label2      = Type
| label2      = Type
| data2        = Anti-ballistic missle
| data2        = Long-range stand-off attack missile
| label3      = Place of origin
| label3      = Place of origin
| data3        = {{team flag|Nouvelle Alexandrie}}
| data3        = {{team flag|Nouvelle Alexandrie}}
Line 16: Line 16:
| data5      = [[Javelin Industries]]
| data5      = [[Javelin Industries]]
| label6      = In service
| label6      = In service
| data6      = {{AN|1680}} - present
| data6      = {{AN|1690}} - present
| label7      = Wars
| label7      = Wars
| data7      = {{Unbulleted list|[[West Baatharzi War]]|[[Second Elwynnese Civil War]]|[[Operation Paramount]]}}
| data7      = {{Unbulleted list|[[Operation Paramount]]}}
| label8      = Mass
| label8      = Weight
| data8        = * 1,300 kg (2,900 lb) ''missile itself''
| data8        = 1,700 kg (3747.85 lbs)
* 2,800 kg (6,200 lb) ''officially''
* 3,500 kg (7,700 lb) ''sealed canister''
| label9      = Length
| label9      = Length
| data9        = 6.8 m (22 ft) – 7 m (23 ft)
| data9        = 6.1m (20.01 ft)
| label10      = Diameter
| label10      = Diameter
| data10        = By stage: 800 mm (31 in) – 1st stage; 500 mm (20 in) – 2nd stage.
| data10        = 0.56m (1.83 ft)
| label11      = Warhead
| label11      = Warhead
| data11        = Directed high explosive fragmentation
| data11        = Options:
* 825x anti-personnel/anti-materiel (APAM) bomblets;
* 12x terminally guided submunition (TGSM);
* 500 kg blast-fragmentation.
| label12      = Detonation mechanism
| label12      = Detonation mechanism
| data12        = Proximity fuse
| data12        = Impact or proximity
| label13      = Engine
| label13      = Engine
| data13        = Two-stage
| data13        = Two-stage
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| data16        = Solid propellant
| data16        = Solid propellant
| label17      = Operational range
| label17      = Operational range
| data17        = 90 km (56 mi) – 150 km (93 mi)
| data17        = 400km (248.5 mi)
| label18      = Flight ceiling
| data18      = Exo-atmospheric
| label19      = Speed
| label19      = Speed
| data19      =  Mach 9, 2.5 km/s (1.6 mi/s)
| data19      =  Mach 6
| label20      = Guidance system
| label20      = Guidance system
| data20      = Dual mode:
| data20      = INS/GPS
* passive infrared seeker;
| label21      = Steering system
* active radar seeker.
| label21      = Guidance system
| data21      = Thrust vectoring and four aerodynamic control moving fins
| data21      = Thrust vectoring and four aerodynamic control moving fins
| label22      = Launch platform
| label22      = Launch platform
| data22      = Six canisters per trailer-mounted erector–launcher
| data22      = Transporter erector launcher
| label23    = Accuracy
| label23    = Accuracy
| data23      = Within 4 m (13 ft) of the target  
| data23      = Within <10 m (32.8 ft) of the target  
}}
}}
[[Category:Missiles]]
[[Category:Javelin Industries]]

Latest revision as of 15:19, 21 November 2022

Mondego (missile)

Mondego 2 Missile, 1698 AN
Type Long-range stand-off attack missile
Place of origin Nouvelle Alexandrie Nouvelle Alexandrie
Designed
Manufacturer Javelin Industries
In service 1690 AN - present
Wars
Weight 1,700 kg (3747.85 lbs)
Length 6.1m (20.01 ft)
Diameter 0.56m (1.83 ft)
Warhead

Options:

  • 825x anti-personnel/anti-materiel (APAM) bomblets;
  • 12x terminally guided submunition (TGSM);
  • 500 kg blast-fragmentation.
Detonation mechanism Impact or proximity
Engine Two-stage
Wingspan 820 mm (32 in)
Propellant Solid propellant
Operational range 400km (248.5 mi)
Speed Mach 6
Guidance system INS/GPS
Steering system Thrust vectoring and four aerodynamic control moving fins
Launch platform Transporter erector launcher
Accuracy Within <10 m (32.8 ft) of the target