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Contents

   



(Top)
 


1 Development  





2 Design overview  





3 Cancellation  





4 See also  





5 Notes  





6 References  





7 External links  














UGM-89 Perseus






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UGM-89A Perseus
TypeStandoff Anti-Submarine & Anti-ship
Place of originUnited States
Service history
Used byUnited States Navy
Production history
ManufacturerLockheed Missiles and Space Company[1]
ProducedCancelled, 1973[2][3][4][5]
Specifications
Mass6,000 lb (2,700 kg)[2][5]
Length25 ft (7.6 m)[2][5]
Diameter30 in (760 mm)[2][5]
WarheadHoming torpedo[2][5]

EngineSolid propellant rocket motor[5][6]

Operational
range

30 nmi (35 mi; 56 km)[2][5]

Launch
platform

Submarine[2][3][4][5]

The UGM-89 Perseus was a proposed U.S. Navy submarine-launched anti-ship (AShM) and anti-submarine (ASW) cruise missile that was developed under the Submarine Tactical Missile (STAM) project, which was also referred to as the Submarine Anti-ship Weapon System (STAWS). This missile system was to be the centerpiece for a proposed third-generation nuclear-powered cruise missile submarine championed by then-Vice Admiral Hyman G. Rickover, the influential but controversial head of the Navy's nuclear propulsion program.[3][4]

Development[edit]

The Navy issued the STAM requirement in March 1969, and the Lockheed Missiles and Space Company (LMSC) responded to this proposal, which included the formation of an undersea warfare program organization in Sunnyvale, California.[1][2][5] It is unclear if this was to be an entirely new organization or part of the Lockheed Underwater Missile Facility (LUMF) which had been responsible for the design and development of the Polaris, Poseidon, and Trident submarine-launched strategic ballistic missile (SLBM) systems for the U.S. Navy.[7] In February 1970, the missile designation ZUGM-89A Perseus was reserved for the U.S. Navy presumably for the STAM/STAWS missile development program.[5][8]

Design overview[edit]

Because of its large size, the UGM-89 Perseus missile could not be launched from the Navy's standard 21 in (530 mm) submarine torpedo tubes, but would be carried in a vertical launching system (VLS) housed within the proposed cruise missile submarine's hull. Twenty VLS tubes would be located in a separate compartment situated between the submarine's operations and reactor compartments.[3][4] The individual launcher tube would be 30 by 300 inches (76 cm × 762 cm) in dimension.[4] The missile warhead payload would be a new 21-inch (533 mm) diameter homing torpedo to be developed concurrently with the UGM-89 Perseus missile.[2][5]

By 1971, the STAM project had evolved into a long-range Advanced Cruise Missile (ACM) program capable of undertaking a variety of combat missions, including strategic nuclear strike (see table below).[4] The proposed ACM versions of the UGM-89 Perseus STAM would use a slightly enlarged launch tube (40 in × 400 in (100 cm × 1,020 cm), and 1979 would have been the date for its initial operational capability (IOC).[4]

1971 ACM Alternatives High-Subsonic Anti-ship/AShW Supersonic Anti-ship/AShW Strategic Nuclear Strike
Dimensions 34 x 336 inches (86.36 x 853.4 cm) 34 x 340 inches (86.36 x 863.6 cm) 34 x 336 inches (86.36 x 853.4 cm)
Overall launch weight 8,600 lbs. (3,900.9 kg) 11,420 lbs. (5,180.0 kg) 9,950 lbs. (4,13.2 kg)
Without booster 6,183 lbs. (2,804.6 kg) 7.519 lbs. (3,410.6 kg) ———
Warhead 1,000 lb. armour piercing (453.6 kg) 700 lb. (317.6 kg) 260 lb. (117.9 kg)
Speed Mach 0.8 (609 mph or 980 km/h) Mach 2.0 (1,522 mph or 2450 km/h) Mach 0.8 (609 mph or 980 km/h)
Range 400 nm (740.8 km) 400 nm (740.8 km) 1800 nm (3,333.6 km)

Cancellation[edit]

The UGM-89 Perseus missile system was cancelled in 1973, and its proposed nuclear-powered cruise missile submarine platform was officially cancelled in 1974, with the Navy deciding to build the less expensive Los Angeles-class nuclear-powered attack submarines, which would subsequently carry both the Harpoon anti-ship missile and Tomahawk cruise missiles.[2][3][4][5] The ASW component of the UGM-89 Perseus would later serve as the baseline for the proposed Sea Lance stand-off ASW missile system, which would also be cancelled.[4][6]

See also[edit]

Notes[edit]

  1. ^ a b "Lockheed's Tactical Undersea Missile". Flight International. 29 May 1969. p. 911. Retrieved 2009-08-26.
  • ^ a b c d e f g h i j "UGM-89 Perseus". Directory of US Military Rockets and Missiles. 24 October 2002. Retrieved 2009-08-26.
  • ^ a b c d e Polmar, Norman; J.K. Moore (2004). Cold War Submarines: The Design and Construction of U.S. and Soviet Submarines. Washington, DC: Potomac Books, Inc. pp. 274–275, 376n40. ISBN 1-57488-530-8. Archived from the original on 2007-10-14. Retrieved 2009-08-26.
  • ^ a b c d e f g h i Friedman, Norman (1994). U.S. Submarines Since 1945: An Illustrated Design History. Annapolis, Maryland: Naval Institute Press. pp. 270–271. ISBN 1-55750-260-9. Retrieved 2009-08-26.
  • ^ a b c d e f g h i j k l "UGM-89 Perseus". Encyclopedia Astronautica. Archived from the original on September 4, 2003. Retrieved 2009-08-26.
  • ^ a b "Boeing RUM/UUM-125 Sea Lance". Directory of US Military Rockets and Missiles. 28 May 2002. Retrieved 2009-08-26.
  • ^ Francillon, René J. (1988). Lockheed Aircraft since 1913. Annapolis, Maryland: Naval Institute Press. pp. Appendix D, p. 558–564. ISBN 0-87021-897-2.
  • ^ "Missile Design Series". Military. GlobalSecurity.org. 2 March 2009. Retrieved 2009-08-26.
  • References[edit]

    External links[edit]


    Retrieved from "https://en.wikipedia.org/w/index.php?title=UGM-89_Perseus&oldid=1189832164"

    Categories: 
    Abandoned military rocket and missile projects of the United States
    Naval guided missile launch systems of the United States
    Cold War anti-submarine weapons of the United States
    Cold War anti-ship missiles of the United States
    Cruise missiles of the United States
    Anti-submarine missiles of the United States
    Lockheed Corporation
    Hidden categories: 
    Articles with short description
    Short description is different from Wikidata
     



    This page was last edited on 14 December 2023, at 08:50 (UTC).

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