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Contents

   



(Top)
 


1 Overview  





2 See also  





3 References  














AIM-97 Seekbat






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From Wikipedia, the free encyclopedia
 


AIM-97 Seekbat
TypeAir-to-air missile
Place of originUnited States
Production history
ManufacturerGeneral Dynamics
Specifications
Mass1,300 pounds (590 kg)
Length15 feet (4.6 m)
Diameter13.5 inches (340 mm)
Wingspan42.5 inches (1,080 mm)
WarheadBlast-fragmentation

EngineAerojet MK 27 dual-thrust solid-fuel rocket

Operational
range

56 miles (90 km)
Flight ceiling80,000 feet (24,000 m)
Maximum speed >Mach3

Guidance
system

Semi-active radar homing (SARH) with terminal infrared homing

Launch
platform

Aircraft

The AIM-97 SeekbatorXAIM-97A Seek Bat was a long-range air-to-air missile developed by the United States. It was intended to counter the perceived capabilities of the Mikoyan-Gurevich MiG-25 and proposed to arm both the F-15 Eagle and F-4 Phantom,[1] the missile ultimately never entered service.

Overview

[edit]

In the early to mid-1970s the United States was highly concerned by the perceived capabilities of the MiG-25, an aircraft which was known to be capable of speeds in excess of Mach 3 and which carried long-range air-to-air missiles.[2] It was widely claimed that the Foxbat was a new generation "super-fighter", capable of comfortably outclassing any US or allied aircraft. The US initiated the F-15 Eagle program largely in response to this threat. To equip the F-15 the Air Force initiated development of the AIM-82 short-range missile and the AIM-97 Seekbat. The former was a dogfighting missile intended as a replacement for the AIM-9 Sidewinder, the latter was to be a new high-altitude long-range missile designed specifically to shoot down the MiG-25 - hence the name "Seekbat", the "bat" referring to the MiG-25's "Foxbat" NATO reporting name.[3]

The Seekbat was based on the AGM-78 Standard ARM. It had a larger[clarification needed] propulsion unit and used semi-active radar homing with an infrared seeker for terminal guidance of the missile.[3] The operational ceiling was 80,000 ft (24,000 m).[2]

Test firings began in late 1972,[a] but the Seekbat program did not make a great deal of progress and was cancelled in 1976.[2] By this time new knowledge of the MiG-25s capabilities and role led to the cancellation of the program because the missile's cost did not justify its procurement.[citation needed]

See also

[edit]

References

[edit]
Notes
  1. ^ Hewish in his March 1974 article states that the missile had been "...undergoing flight-test for more than a year."[3]
  • ^ a b c Hewish 1974, p. A16
  • Bibliography

    Retrieved from "https://en.wikipedia.org/w/index.php?title=AIM-97_Seekbat&oldid=1117608556"

    Categories: 
    General Dynamics
    Proposed weapons of the United States
    Cold War air-to-air missiles of the United States
    Abandoned military rocket and missile projects of the United States
    Hidden categories: 
    Articles needing additional references from September 2016
    All articles needing additional references
    Articles with short description
    Short description matches Wikidata
    Wikipedia articles needing clarification from September 2015
    All articles with unsourced statements
    Articles with unsourced statements from September 2016
     



    This page was last edited on 22 October 2022, at 16:54 (UTC).

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