>soviet union >short-range air-to-air missile >in service

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>soviet union
>short-range air-to-air missile
>in service 1960
>weight 90 kg (200 lb) (R-13M)
>length 2.830 m (9 ft 3.4 in) (R-13M) 3.48 m (11 ft 5 in) (R-3R)
>diameter 127 mm (5.0 in)
>warhead 7.4 kg (16 lb)
>solid-fuel rocket engine
>wingspan 631 mm (24.8 in) (R-13M)
>operational range 1.0 to 35.4 kilometres (0.6 to 22 mi)
>speed Mach 2.5.
>guidance system infrared homing
>launch platform MiG-21, MiG-23, Sukhoi Su-17/20/22.

The missile knows where it is at all times. It knows this because it knows where it isn't. By subtracting where it is from where it isn't, or where it isn't from where it is (whichever is greater), it obtains a difference, or deviation. The guidance subsystem uses deviations to generate corrective commands to drive the missile from a position where it is to a position where it isn't, and arriving at a position where it wasn't, it now is. Consequently, the position where it is, is now the position that it wasn't, and it follows that the position that it was, is now the position that it isn't.
In the event that the position that it is in is not the position that it wasn't, the system has acquired a variation, the variation being the difference between where the missile is, and where it wasn't. If variation is considered to be a significant factor, it too may be corrected by the GEA. However, the missile must also know where it was.

The missile guidance computer scenario works as follows. Because a variation has modified some of the information the missile has obtained, it is not sure just where it is. However, it is sure where it isn't, within reason, and it knows where it was. It now subtracts where it should be from where it wasn't, or vice-versa, and by differentiating this from the algebraic sum of where it shouldn't be, and where it was, it is able to obtain the deviation and its variation, which is called error.

File: AA-2 ATOLL..jpg (211KB, 768x380px) Image search: [Google]

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>soviet union
>short-range air-to-air missile
>in service 1960
>weight 90 kg (200 lb) (R-13M)
>length 2.830 m (9 ft 3.4 in) (R-13M) 3.48 m (11 ft 5 in) (R-3R)
>diameter 127 mm (5.0 in)
>warhead 7.4 kg (16 lb)
>solid-fuel rocket engine
>wingspan 631 mm (24.8 in) (R-13M)
>operational range 1.0 to 35.4 kilometres (0.6 to 22 mi)
>speed Mach 2.5
>guidance system infrared homing..
>launch platform MiG-21, MiG-23, Sukhoi Su-17/20/22

>>4292555
wow

File: K-13 (AA-2_'Atoll').jpg.jpg (5KB, 250x166px) Image search: [Google]

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>soviet union
>short-range air-to-air missile
>in service 1960
>weight 90 kg (200 lb) (R-13M)
>length 2.830 m (9 ft 3.4 in) (R-13M) 3.48 m (11 ft 5 in) (R-3R)
>diameter 127 mm (5.0 in)
>warhead 7.4 kg (16 lb)
>solid-fuel rocket engine
>wingspan 631 mm (24.8 in) (R-13M)
>operational range 1.0 to 35.4 kilometres (0.6 to 22 mi)
>speed Mach 2.5
>guidance system infrared homing.
>launch platform MiG-21, MiG-23, Sukhoi Su-17/20/22.

File: AIM_9L_Sidewinder_p1220802.jpg (2MB, 2560x1920px) Image search: [Google]

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>United States
>short-range air-to-air missile
>in service 1956
>weight 8.53 kg (188 lb)
>length 3.02 m (9 ft 11 in)
>diameter 127 mm (5.0 in)
>warhead 9.4 kg (20.8 lb)
>solid-fuel rocket engine
>wingspan 279.4 mm (11 in)
>operational range 1.0 to 35.4 km (0.6 to 22 miles)
>speed Mach 2.7
>guidance system infrared homing.
>launch platform aircraft

>>4292826
K-13 AA-2 Atoll >>> AIM-9 Sidewinder.

>>4292900
>00
dubs confirm WW3 Victory to RUssia

File: Naval Strike Missile (NSM).jpg (29KB, 800x233px) Image search: [Google]

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>Norway
>littoral/open sea anti-ship/land attack cruise missile
>in service 2012
>weight 410 kg (900 lb)
>length 3.95 m (13.0 ft)
>warhead 125 kg (276 lb) HE blast-fragmentation
>engine solid fuel rocket booster, microturbo TRI 40 turbojet
>operational range NSM 185 km (115 mi; 100 nmi)+, JSM 290 km (180 mi; 160 nmi)+
>flight altitude sea skimming
>speed high subsonic
>guidance system inertial, GPS, terrain-reference navigation, imaging infrared homing, target database
>launch platform naval ships, land-based vehicles

File: AIM-120 AMRAAM.jpg (231KB, 1280x853px) Image search: [Google]

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>United States
>Medium-range, active radar homing air-to-air missile
>Weight 335 pounds (152 kg)
>Length 12 feet (3.7 m)
>Diameter 7 inches (180 mm)
>Warhead High explosive blast-fragmentation • AIM-120A/B: WDU-33/B, 50 pounds (22.7 kg) • AIM-120C-5: WDU-41/B, 40 pounds (18.1 kg)
>Detonation mechanism Active RADAR Target Detection Device (TDD) Quadrant Target Detection Device (QTDD) in AIM-120C-6 – lots 13+
>Engine Solid-fuel rocket motor
>Wingspan 20.7 inches (530 mm) (AIM-120A/B)
>Operational range • AIM-120A/B: 55–75 km (30–40 nmi) • AIM-120C-5: >105 km (>57 nmi) • AIM-120D (C-8): >160 km (>97 nmi)
>Speed Mach 4 (4,900 km/h; 3,045 mph; 1.3612 km/s)
>Guidance system inertial guidance, terminal active radar homing
>Launch platform aircraft, surface-launched

File: Kaliningrand K-5 (AA1-ALKALI).jpg (217KB, 800x531px) Image search: [Google]

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>soviet union
>short-range air-to-air missile
>in service 1957
>weight 82.7 kg (182 lb)
>length 2.49 m (8 ft 2 in)
>diameter 200 mm (7.9 in)
>warhead High explosive
>warhead weight 13 kg (29 lb)
>engine Rocket
>operational range 2 to 6 kilometres (1.2 to 3.7 mi)
>speed 2,880 km/h (1,790 mph)
>guidance system beam riding
>launch platform MiG-17, MiG-19, MiG-21, Su-9

File: K-13 (missile) AA-2 ATOLL.jpg (288KB, 1000x524px) Image search: [Google]

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>>4292555
BEST GIRL
E
S
T

G
I
R
L

File: 800px-Howell_torpedo.jpg (74KB, 800x529px) Image search: [Google]

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>united states
>anti-surface ship torpedo
>in service 1890–1898
>weight 580 lbs[2]
>length 132 inches[2]
>diameter 14.2 inches
>effective firing range 400 yards
>warhead wet guncotton
>warhead weight 100 lbs
>detonation mechanism contact device
>engine flywheel
>speed 25 knots
>launch platform battleships and torpedo boats

File: P-700 Granit (SS-N-19 Shipwreck).jpg (45KB, 270x200px) Image search: [Google]

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>Soviet union
>long-range anti-ship cruise missile
>in service 1983
>weight 7,000 kg (15,400 lb)
>length 10 m (33 ft)
>diameter 0.85 m (33 in)
>warhead High explosive or nuclear
>warhead weight 750 kg (1,653 lb) HE (unknown composition, probably RDX or similar) or 500 kt fission-fusion thermonuclear weapon
>blast yield 500 kt
>engine ramjet
>operational range 625 km (388 mi)
>speed Mach 1.6 (low altitude) - 2.5+ (high altitude)
>guidance system inertial guidance, active radar homing with home-on-jam, and Legenda satellite targeting system (believed to be nonfunctional after the fall of the USSR)
>launch platform oscar class submarines kirov & admiral Kuznetsov class ships

desu

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mabe