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Short-Range Air-to-Air Missiles
Raven™ Short-Range Air-to-Air Missile
Physical properties
Mass: [kg] 44
Mass at end of booster burn: [kg] 34
Calibre: [mm] 120
Length: [m] 2.095
Engine properties
Build: Delta 15 Ripple Lake™ Solid-Fuel, manufactured by Crown Jewel Motors™
Force exerted by booster: [N] 9,500
Burn time of booster: [s] 3
Raw acceleration at ignition: [m/s²] 215.91
Specific impulse of booster: [s] 290.52
ΔV of booster: [m/s] 734.81
Booster start delay: [s] 0
Total ΔV: [m/s] 734.81
Fuse and warhead properties
Explosive mass: [kg of TNT equivalent] 1.35
Proximity fuse: Yes
Proximity fuse range: [m] 3
Proximity fuse shell detection (80-200 mm): Yes
Proximity fuse delay: [s] 0.5
Guidance properties
Guidance type: Infrared
Guidance start delay: [s] 0.35
Guidance duration: [s] 25
Seeker warm up time: [s] 1
Seeker search duration: [s] 20
Field of view: [degrees] 5
Gimbal limit: [degrees] 45
Track rate: [degrees/second] 35
Uncaged seeker before launch: Yes
Maximum lock angle before launch: [degrees] 17
Minimum angle of incidence of the seeker to the Sun for it to not capture the Sun: [degrees] 7
Lock-on range from rear-aspect: [km] 7.4
Flare and IRCM detection range: [km] 7.4
Head-on lock-on range against afterburning target: 3
Maximum break lock time: [s] 3
Can be slaved to radar: Yes
Proportional navigation multiplier: (affects how far ahead it attempts to lead) 4
Base indicated air speed: [m/s] 1,800
Flight characteristics
Maximum fin angle of attack: [degrees] 16.2
Maximum fin lateral acceleration: 21.5
Wing area multiplier: 1.29
Minimum range: [m] 30
Maximum (flight) range: [km] 15
Maximum G-load: [G] 30
Price: $39,250.00
Crow™ Short-Range Air-to-Air Missile
Physical properties
Mass: [kg] 105
Mass at end of booster burn: [kg] 71
Calibre: [mm] 170
Length: [m] 2.9
Engine properties
Build: Delta Rush™ Solid-Fuel, manufactured by Crown Jewel Motors™
Force exerted by booster: [N] 13,736
Burn time of booster: [s] 5.5
Raw acceleration at ignition: [m/s²] 130.82
Specific impulse of booster: [s] 226.50
ΔV of booster: [m/s] 869.43
Booster start delay: [s] 0
Total ΔV: [m/s] 869.43
Fuse and warhead properties
Explosive mass: [kg of TNT equivalent] 5.94
Proximity fuse: Yes
Proximity fuse range: [m] 3
Proximity fuse shell detection (80-200 mm): Yes
Proximity fuse delay: [s] 0.5
Guidance properties
Guidance type: Infrared
Guidance start delay: [s] 0.3
Guidance duration: [s] 23
Seeker warm up time: [s] 1
Seeker search duration: [s] 20
Field of view: [degrees] 4.5
Gimbal limit: [degrees] 75
Track rate: [degrees/second] 60
Uncaged seeker before launch: Yes
Maximum lock angle before launch: [degrees] 45
Minimum angle of incidence of the seeker to the Sun for it to not capture the Sun: [degrees] 15
Lock-on range from rear-aspect: [km] 11
Flare range: [km] 11
Head-on lock-on range against afterburning target: 6
Maximum break lock time: [s] 3
Can be slaved to radar: Yes
Proportional navigation multiplier: (affects how far ahead it attempts to lead) 7
Base indicated air speed: [m/s] 3,000
Flight characteristics
Maximum fin angle of attack: [degrees] 22.5
Maximum fin lateral acceleration: 45
Wing area multiplier: 1.5
Minimum range: [m] 30
Maximum (flight) range: [km] 25
Maximum G-load: [G] 30
Price: $50,250.00
Condor™ Short-Range Air-to-Air Missile
Physical properties
Mass: [kg]
Mass at end of booster burn: [kg]
Calibre: [mm]
Length: [m]
Engine properties
Build: manufactured by Crown Jewel Motors™
Force exerted by booster: [N]
Burn time of booster: [s]
Raw acceleration at ignition: [m/s²]
Specific impulse of booster: [s]
ΔV of booster: [m/s]
Booster start delay: [s]
Total ΔV: [m/s]
Fuse and warhead properties
Explosive mass: [kg of TNT equivalent]
Proximity fuse:
Proximity fuse range: [m]
Proximity fuse shell detection (80-200 mm):
Proximity fuse delay: [s]
Guidance properties
Guidance type: Infrared
Guidance start delay: [s]
Guidance duration: [s]
Seeker warm up time: [s]
Seeker search duration: [s]
Field of view: [degrees]
Gimbal limit: [degrees]
Track rate: [degrees/second]
Uncaged seeker before launch:
Maximum lock angle before launch: [degrees]
Minimum angle of incidence of the seeker to the Sun for it to not capture the Sun: [degrees]
Lock-on range from rear-aspect: [km]
Flare and IRCM detection range: [km]
Head-on lock-on range against afterburning target:
Maximum break lock time: [s]
Can be slaved to radar:
Proportional navigation multiplier: (affects how far ahead it attempts to lead)
Base indicated air speed: [m/s]
Flight characteristics
Maximum fin angle of attack: [degrees]
Maximum fin lateral acceleration:
Wing area multiplier:
Maximum speed: [m/s]
Flight time until guidance starts (delay): [s]
Flight time when pull limit reaches 100%: [s]
Minimum range: [m]
Maximum (flight) range: [km]
Maximum G-load: [G]
Price: $72,675.00
Falcon™ Short-Range Air-to-Air Missile
Physical properties
Mass: [kg]
Mass at end of booster burn: [kg]
Calibre: [mm]
Length: [m]
Engine properties
Build: manufactured by Crown Jewel Motors™
Force exerted by booster: [N]
Burn time of booster: [s]
Raw acceleration at ignition: [m/s²]
Specific impulse of booster: [s]
ΔV of booster: [m/s]
Booster start delay: [s]
Total ΔV: [m/s]
Fuse and warhead properties
Explosive mass: [kg of TNT equivalent]
Proximity fuse:
Proximity fuse range: [m]
Proximity fuse shell detection (80-200 mm):
Proximity fuse delay: [s]
Guidance properties
Guidance type: Infrared
Guidance start delay: [s]
Guidance duration: [s]
Seeker warm up time: [s]
Seeker search duration: [s]
Field of view: [degrees]
Gimbal limit: [degrees]
Track rate: [degrees/second]
Uncaged seeker before launch:
Maximum lock angle before launch: [degrees]
Minimum angle of incidence of the seeker to the Sun for it to not capture the Sun: [degrees]
Lock-on range from rear-aspect: [km]
Flare and IRCM detection range: [km]
Head-on lock-on range against afterburning target:
Maximum break lock time: [s]
Can be slaved to radar:
Proportional navigation multiplier: (affects how far ahead it attempts to lead)
Base indicated air speed: [m/s]
Flight characteristics
Maximum fin angle of attack: [degrees]
Maximum fin lateral acceleration:
Wing area multiplier:
Maximum speed: [m/s]
Flight time until guidance starts (delay): [s]
Flight time when pull limit reaches 100%: [s]
Minimum range: [m]
Maximum (flight) range: [km]
Maximum G-load: [G]
Price: $88,125.00
Raven II™ Short-Range Air-to-Air Missile
Physical properties
Mass: [kg]
Mass at end of booster burn: [kg]
Calibre: [mm]
Length: [m]
Engine properties
Build: manufactured by Crown Jewel Motors™
Force exerted by booster: [N]
Burn time of booster: [s]
Raw acceleration at ignition: [m/s²]
Specific impulse of booster: [s]
ΔV of booster: [m/s]
Booster start delay: [s]
Total ΔV: [m/s]
Fuse and warhead properties
Explosive mass: [kg of TNT equivalent]
Proximity fuse:
Proximity fuse range: [m]
Proximity fuse shell detection (80-200 mm):
Proximity fuse delay: [s]
Guidance properties
Guidance type: Infrared
Guidance start delay: [s]
Guidance duration: [s]
Seeker warm up time: [s]
Seeker search duration: [s]
Field of view: [degrees]
Gimbal limit: [degrees]
Track rate: [degrees/second]
Uncaged seeker before launch:
Maximum lock angle before launch: [degrees]
Minimum angle of incidence of the seeker to the Sun for it to not capture the Sun: [degrees]
Lock-on range from rear-aspect: [km]
Flare and IRCM detection range: [km]
Head-on lock-on range against afterburning target:
Maximum break lock time: [s]
Can be slaved to radar:
Proportional navigation multiplier: (affects how far ahead it attempts to lead)
Base indicated air speed: [m/s]
Flight characteristics
Maximum fin angle of attack: [degrees]
Maximum fin lateral acceleration:
Wing area multiplier:
Maximum speed: [m/s]
Flight time until guidance starts (delay): [s]
Flight time when pull limit reaches 100%: [s]
Minimum range: [m]
Maximum (flight) range: [km]
Maximum G-load: [G]
Price: $94,720.00
Vulture™ Short-Range Air-to-Air Missile
Physical properties
Mass: [kg]
Mass at end of booster burn: [kg]
Calibre: [mm]
Length: [m]
Engine properties
Build: manufactured by Crown Jewel Motors™
Force exerted by booster: [N]
Burn time of booster: [s]
Raw acceleration at ignition: [m/s²]
Specific impulse of booster: [s]
ΔV of booster: [m/s]
Booster start delay: [s]
Total ΔV: [m/s]
Fuse and warhead properties
Explosive mass: [kg of TNT equivalent]
Proximity fuse:
Proximity fuse range: [m]
Proximity fuse shell detection (80-200 mm):
Proximity fuse delay: [s]
Guidance properties
Guidance type: Infrared
Guidance start delay: [s]
Guidance duration: [s]
Seeker warm up time: [s]
Seeker search duration: [s]
Field of view: [degrees]
Gimbal limit: [degrees]
Track rate: [degrees/second]
Uncaged seeker before launch:
Maximum lock angle before launch: [degrees]
Minimum angle of incidence of the seeker to the Sun for it to not capture the Sun: [degrees]
Lock-on range from rear-aspect: [km]
Flare and IRCM detection range: [km]
Head-on lock-on range against afterburning target:
Maximum break lock time: [s]
Can be slaved to radar:
Proportional navigation multiplier: (affects how far ahead it attempts to lead)
Base indicated air speed: [m/s]
Flight characteristics
Maximum fin angle of attack: [degrees]
Maximum fin lateral acceleration:
Wing area multiplier:
Maximum speed: [m/s]
Flight time until guidance starts (delay): [s]
Flight time when pull limit reaches 100%: [s]
Minimum range: [m]
Maximum (flight) range: [km]
Maximum G-load: [G]
Price: $102,330.00
Medium-Range Air-to-Air Missiles
L1™ Air-to-Air Missile
The L1 Air-to-Air Missile is not guided by the actual position recorded by the detector, but by the change in position since the last sighting. So if the target remained at 5 degrees left between two rotations of the mirror, the electronics would not output any signal to the control system. Consider a missile fired at right angles to its target; if the missile is flying at the same speed as the target, it should "lead" it by 45 degrees, flying to an impact point far in front of where the target was when it was fired. If the missile is traveling four times the speed of the target, it should follow an angle about 11 degrees in front. In either case, the missile should keep that angle all the way to interception, which means that the angle that the target makes against the detector is constant.This "proportional pursuit" system is straightforward to implement and offers high-performance lead calculation almost for free and can respond to changes in the target's flight path, which is much more efficient and makes the missile "lead" the target.
Physical properties
Mass: [kg] 84.46
Mass at end of booster burn: [kg] 57.06
Calibre: [mm] 127
Length: [m] 2.85
Engine properties
Build: Silver back Mk. 36™ solid-fuel, manufactured by Crown Jewel Motors™
Force exerted by booster: [N] 10800
Burn time of booster: [s] 5.3
Raw acceleration at ignition: [m/s²] 127.87
Specific impulse of booster: [s] 212.95
ΔV of booster: [m/s] 819.27
Booster start delay: [s] 0
Total ΔV: [m/s] 819.27
Fuse and warhead properties
Explosive mass: [kg of TNT equivalent] 4.064
Proximity fuse: Yes
Proximity fuse range: [m] 5
Proximity fuse shell detection (80-200 mm): Yes
Proximity fuse delay: [s] 0.5
Guidance properties
Guidance type: Infrared
Guidance start delay: [s] 0.5
Guidance duration: [s] 60
Seeker warm up time: [s] 1
Seeker search duration: [s] 20
Field of view: [degrees] 3.6
Gimbal limit: [degrees] 45
Track rate: [degrees/second] 22
Uncaged seeker before launch: Yes
Maximum lock angle before launch: [degrees] 40
Minimum angle of incidence of the seeker to the Sun for it to not capture the Sun: [degrees] 10
Lock-on range from rear-aspect: [km] 3
Flare and IRCM detection range: [km] 11
Head-on lock-on range against afterburning target: [km] 6
Maximum break lock time: [s] 3
Can be slaved to radar: Yes
Proportional navigation multiplier: (affects how far ahead it attempts to lead) 4
Base indicated air speed: [m/s] 1800
Flight characteristics
Maximum fin angle of attack: [degrees] 24.3
Maximum fin lateral acceleration: 37.5
Wing area multiplier: 1.4
Maximum speed: [m/s] 1000
Minimum range: [m] 30
Maximum (flight) range: [km] 18
Maximum G-load: [G] 30
Price: $399,500.00
Clear Cap™ Medium-Range Air-to-Air Missile
The Clear Cap was designed to intercept agile and maneuvering aircraft and cruise missiles, particularly low-flying targets. It has four clipped triangular fixed stabilizers at the front, four clipped delta-wings and four moving clipped-tip raked control fins at the rear. This missile is 4.16m long, has a body diameter of 200mm, and a wingspan of 1.04m.
The earlier Clear Cap missiles had a launch weight of 222kg and a maximum range of 25km with a 25kg HE fragmentation warhead. This missile has command mid-course guidance and a tail aspect IR seeker.
Physical properties
Mass: [kg] 215
Mass at end of booster burn: [kg] 182
Calibre: [mm] 200
Length: [m] 4.16
Engine properties
Build: X-10 Giancarlo Classic™ Solid-Fuel, manufactured by Crown Jewel Motors™
Force exerted by booster: [N] 60,000
Burn time of booster: [s] 1.85
Raw acceleration at ignition: [m/s²] 279.07
Specific impulse of booster: [s] 342.88
ΔV of booster: [m/s] 560.49
Booster start delay: [s] 0
Total ΔV: [m/s] 460.49
Fuse and warhead properties
Explosive mass: [kg of TNT equivalent] 20.8
Proximity fuse: Yes
Proximity fuse range: [m] 10
Proximity fuse shell detection (80-200 mm): Yes
Proximity fuse delay: [s] 1
Guidance properties
Guidance type: Infrared
Guidance start delay: [s] 0.5
Guidance duration: [s] 35
Seeker warm up time: [s] 1
Seeker search duration: [s] 20
Field of view: [degrees] 2.6
Gimbal limit: [degrees] 60
Track rate: [degrees/second] 12
Uncaged seeker before launch: Yes
Maximum lock angle before launch: [degrees] 60
Minimum angle of incidence of the seeker to the Sun for it to not capture the Sun: [degrees] 7
Lock-on range from rear-aspect: [km] 12
Flare and IRCM detection range: [km] 12
Head-on lock-on range against afterburning target: [km] 4
Maximum break lock time: [s] 3
Can be slaved to radar: Yes
Proportional navigation multiplier: 4
Base indicated air speed: [m/s] 1800
Flight characteristics
Maximum fin angle of attack: [degrees] 18.9
Maximum fin lateral acceleration: 15.9
Wing area multiplier: 1.35
Maximum speed: [m/s] 1,000
Flight time until guidance starts (delay): [s] 0.5
Flight time when pull limit reaches 100%: [s] 2.5
Minimum range: [m] 30
Maximum (flight) range: [km] 27
Price: $425,700.00
White Cap X-11™ Medium-Range Air-to-Air Missile
Physical properties
Mass: [kg] 237
Mass at end of booster burn: [kg] 162
Calibre: [mm] 200
Length: [m] 4.194
Engine properties
Build: X-11 Giancarlo II™ Solid-Fuel, manufactured by Crown Jewel Motors™
Force exerted by booster: [N] 50,000
Burn time of booster: [s] 3
Raw acceleration at ignition: [m/s²] 210.97
Specific impulse of booster: [s] 203.87
ΔV of booster: [m/s] 760.93
Booster start delay: [s] 0
Total ΔV: [m/s] 760.93
Fuse and warhead properties
Explosive mass: [kg of TNT equivalent] 20.8
Proximity fuse: Yes
Proximity fuse range: [m] 10
Proximity fuse shell detection (80-200 mm): Yes
Proximity fuse delay: [s] 1
Guidance properties
Guidance type: Infrared
Guidance start delay: [s] 0.5
Guidance duration: [s] 45
Seeker warm up time: [s] 1
Seeker search duration: [s] 20
Field of view: [degrees] 2.6
Gimbal limit: [degrees] 55
Track rate: [degrees/second] 20
Uncaged seeker before launch: Yes
Maximum lock angle before launch: [degrees] 55
Minimum angle of incidence of the seeker to the Sun for it to not capture the Sun: [degrees] 7
Lock-on range from rear-aspect: [km] 16
Flare and IRCM detection range: [km] 15
Head-on lock-on range against afterburning target: [km] 8
Maximum break lock time: [s] 3
Can be slaved to radar: Yes
Proportional navigation multiplier: (affects how far ahead it attempts to lead) 4
Base indicated air speed: [m/s] 1,800
Flight characteristics
Maximum fin angle of attack: [degrees] 25.2
Maximum fin lateral acceleration: 21.9
Wing area multiplier: 1.35
Maximum speed: [m/s] 1,500
Flight time when pull limit reaches 100%: [s] 1
Minimum range: [m] 30
Maximum (flight) range: [km] 45
Maximum G-load: [G] 24
Price: $438,100.00
Red Cap™ Medium-Range Air-to-Air Missile
Physical properties
Mass: [kg] 245
Mass at end of booster burn: [kg] 177
Calibre: [mm] 230
Length: [m] 3.7
Engine properties
Build: X-12 Giancarlo III™ Sold-Fuel, manufactured by Crown Jewel Motors™
Force exerted by booster: [N] 26,000
Burn time of booster: [s] 6
Raw acceleration at ignition: [m/s²] 106.12
Specific impulse of booster: [s] 235.59
ΔV of booster: [m/s] 744.84
Booster start delay: [s] 0
Total ΔV: [m/s]744.84
Fuse and warhead properties
Explosive mass: [kg of TNT equivalent] 24
Proximity fuse: Yes
Proximity fuse range: [m] 10
Proximity fuse shell detection (80-200 mm): Yes
Proximity fuse delay: [s] 1.7
Guidance properties
Guidance type: Infrared
Guidance start delay: [s] 0.35
Guidance duration: [s] 60
Seeker warm up time: [s] 1
Seeker search duration: [s] 20
Field of view: [degrees] 2
Gimbal limit: [degrees] 55
Track rate: [degrees/second] 30
Uncaged seeker before launch: Yes
Maximum lock angle before launch: [degrees] 50
Minimum angle of incidence of the seeker to the Sun for it to not capture the Sun: [degrees] 5
Lock-on range from rear-aspect: [km] 18
Flare and IRCM detection range: [km] 16
Head-on lock-on range against afterburning target: Yes
Maximum break lock time: [s] 3
Can be slaved to radar: Yes
Proportional navigation multiplier: (affects how far ahead it attempts to lead) 4
Base indicated air speed: [m/s] 1,800
Flight characteristics
Maximum fin angle of attack: [degrees] 25.2
Maximum fin lateral acceleration: 25
Wing area multiplier: 1.4
Maximum speed: [m/s] 1,500
Flight time until guidance starts (delay): [s] 0.35
Flight time when pull limit reaches 100%: [s] 0.4
Minimum range: [m] 20
Maximum (flight) range: [km] 50
Maximum G-load: [G] 30
Price: $472,100.00
Ivory Cap™ Medium-Range Air-to-Air Missile
Physical properties
Mass: [kg] 343
Mass at end of booster burn: [kg] 279
Calibre: [mm] 260
Length: [m] 4.5
Engine properties
Build: X-12+ Giancarlo III™ Solid-Fuel, manufactured by Crown Jewel Motors™
Force exerted by booster: [N] 73,600
Burn time of booster: [s] 2
Raw acceleration at ignition: [m/s²] 214.58
Specific impulse of booster: [s] 234.45
ΔV of booster: [m/s] 474.99
Booster start delay: [s] 0
Total ΔV: [m/s] 1,227.60
Fuse and warhead properties
Explosive mass: [kg of TNT equivalent] 24
Proximity fuse: Ye
Proximity fuse range: [m] 10
Proximity fuse shell detection (80-200 mm): Yes
Proximity fuse delay: [s] 1.7
Guidance properties
Guidance type: Infrared
Guidance start delay: [s] 0.35
Guidance duration: [s] 60
Seeker warm up time: [s] 1
Seeker search duration: [s] 20
Field of view: [degrees] 2
Gimbal limit: [degrees] 55
Track rate: [degrees/second] 30
Uncaged seeker before launch: Yes
Maximum lock angle before launch: [degrees] 50
Minimum angle of incidence of the seeker to the Sun for it to not capture the Sun: [degrees] 5
Lock-on range from rear-aspect: [km] 18
Flare and IRCM detection range: [km] 16
Head-on lock-on range against afterburning target: 8.4
Maximum break lock time: [s] 3
Can be slaved to radar: Yes
Proportional navigation multiplier: (affects how far ahead it attempts to lead) 4
Base indicated air speed: [m/s] 1,800
Flight characteristics
Maximum fin angle of attack: [degrees] 25.2
Maximum fin lateral acceleration: 25
Wing area multiplier: 1.4
Maximum speed: [m/s] 1,700
Flight time until guidance starts (delay): [s] 0.35
Flight time when pull limit reaches 100%: [s] 0.4
Minimum range: [m] 20
Maximum (flight) range: [km] 67.5
Maximum G-load: [G] 30
Price: $514,640.00
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