KS-1 Komet
A Comprehensive Analysis of the Soviet Air-Launched Anti-Ship Missile System.
System Overview ℹ️ Technical Details 📏Dive in with Flashcard Learning!
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System Overview
The Komet Missile
The Raduga KS-1 Komet, designated AS-1 'Kennel' by NATO, was a Soviet short-range air-to-surface missile primarily developed for anti-ship missions. It represented an early foray into guided missile technology for strategic air power, designed to be carried by strategic bombers.
Aircraft Integration
The KS-1 was integrated onto two prominent Soviet aircraft: the Tupolev Tu-4 and the Tupolev Tu-16 strategic bombers. This allowed for standoff engagement capabilities against naval targets, a critical aspect of Cold War military doctrine.
Origin and Service
Developed in the Soviet Union, the KS-1 Komet entered service around 1953, with its operational deployment continuing until 1969. Its design drew heavily from contemporary fighter aircraft aerodynamics, reflecting the era's approach to missile development.
Development & Design
Design Philosophy
Development commenced in 1947, concurrently with a related ground-launched variant, the SSC-2B "Samlet" (S-2 Sopka). Both missiles utilized aerodynamic principles derived from the Mikoyan-Gurevich MiG-15 fighter aircraft, essentially a scaled-down, un-manned version. This approach leveraged existing aerodynamic knowledge and manufacturing capabilities.
Propulsion and Guidance
The KS-1 was propelled by a Klimov RD-500K turbojet engine, a Soviet reverse-engineering of the British Rolls-Royce Derwent. Its guidance system comprised an inertial navigation system (INS) for mid-course correction, transitioning to active radar homing for terminal guidance, enabling it to track and engage moving targets.
Armament
The missile was equipped with a substantial 600 kg (1,300 lb) high-explosive warhead, designed for significant impact against naval vessels. Its operational range extended up to 100 kilometers, providing a crucial standoff capability for its carrier aircraft.
Technical Specifications
Dimensions & Mass
Mass: 3,000 kg (6,600 lb)
Length: 8.29 m (27 ft 2 in)
Diameter: 1.20 m (3 ft 11 in)
Wingspan: 4.77 m (15 ft 8 in)
Performance
Engine: RD-500K turbojet
Operational Range: 90 km (56 mi) to 100 km
Maximum Speed: Mach 0.9
Guidance & Payload
Guidance System: Inertial navigation (midcourse), Active radar homing (terminal)
Warhead: 600 kg (1,300 lb) High Explosive
Launch Platforms
Primary: Tupolev Tu-16 'Badger'
Secondary: Tupolev Tu-4 (K variant only)
Variants & Derivatives
S-2 Sopka (SSC-2b Samlet)
The Sopka was a coastal defense variant, identified by NATO as SSC-2b "Samlet." It utilized a SPRD-15 jet-assisted rocket for initial launch velocity from fixed ground launchers, allowing the KS-1's turbojet to take over. This system was deployed for land-based attacks on maritime targets and saw service in Eastern Bloc nations, including a notable deployment in Cuba during the Cold War and use by Egypt in the Yom Kippur War. It remained in service until approximately 1980.
FKR-1 (SSC-2a Salish)
Designated FKR-1 (Frontline Combat Rocket) and codenamed "Salish" by NATO (SSC-2a), this was a mobile, nuclear-capable variant. It entered service in 1957 with Soviet and East German forces. Featuring a 12-kiloton warhead and an extended range of up to 180 km, it was modified to accept tactical nuclear warheads. The FKR system was positioned in Cuba during the Cuban Missile Crisis, equipped with nuclear warheads, highlighting its strategic significance.
Former Operators
Global Deployment
The KS-1 Komet and its variants were operated by several nations during the Cold War and its aftermath:
Cuba (Sopka variant)
Egypt (Air Force)
Indonesia (Air Force)
Soviet Union (Long Range Aviation, Air Forces)
North Korea
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Important Notice
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