| SUM-N-2 Grebe | |
| Origin: | United States |
| Is Missile: | yes |
| Design Date: | 1947–1950 |
| Service: | 1950 |
| Number: | 20 |
| Weight: | Rocket powered, 2500lb Pulsejet powered, |
| Diameter: | 21inches |
| Length: | 16inchesft5inchesin (ftin) |
| Engine: | Solid-propellant rocket booster McDonnell pulsejet sustainer optional |
| Vehicle Range: | Rocket powered, 5000yd Pulsejet powered, 40000yd |
| Speed: | Mach 0.5 |
The SUM-N-2 Grebe, also known as Kingfisher E and SUM-2, was a rocket- and pulsejet-powered anti-ship and anti-submarine missile developed by the United States Navy in the late 1940s. Intended to allow a ship to deliver a torpedo at a significant distance from the launch location, it proved impractical in trials, and did not enter operational service.
Grebe was developed as part of Project Kingfisher, a program administered by the National Bureau of Standards for the development of a family of torpedo-carrying missiles, allowing underwater-striking weapons to be delivered at stand-off distance from their launching platform. The program developed three air-launched weapons, initially designated Kingfisher C, D, and F; the sole surface-launched member of the family to reach the development stage was Kingfisher E, with development work beginning in 1946.[1]
Kingfisher E, redesignated SUM-2 in September 1947 and SUM-N-2 Grebe in 1948, was a bulky yet conventionally-configured missile resembling a small unmanned aircraft, with a high-mounted, straight wing of span and a twin tail empennage configuration.[2] Constructed by the Goodyear Aircraft Company under subcontract to the Bureau of Standards, the missile was 16feet in length, in diameter and weighed at launch.[2] Power was provided initially by a solid-propellant rocket, giving a range of 5000yd at Mach 0.5; later in the design process a variant with a pulsejet sustainer engine was designed, weighing and boosting the missile's range to 40000yd at a cruising speed of Mach 0.26.[3]
The original specification for the missile called for the Mark 35 torpedo to serve as the SUM-N-2's payload; later, to reduce weight, the design was changed to use the Mark 41 torpedo.[4] Several forms of guidance were evaluated, although none had been definitively selected by the end of the program; the torpedo utilized acoustic homing for terminal guidance.[5]
Given the cover designation of "AA Target Mk 52 Mod 2",[2] testing of the XSUM-N-2 prototype missiles began in early 1950.[2] Twenty airframes were constructed for use in the testing program;[6] by 1953, however, the program had been cancelled; the stated reason for the cancellation was that the missile outranged the sonar equipment that was required to find targets for it, thus making it infeasible to use at its maximum range.[1] Although the concept of a torpedo-carrying pilotless aircraft failed to find favor with the U.S. Navy, the later French Malafon and Australian Ikara missiles are remarkably similar in concept and configuration;[4] the U.S. Navy would later develop the RUR-5 ASROC, a rocket-delivered torpedo (or a pure missile in the nuclear version), for attacking submarines at range.[6]
In 1972, one Grebe was refurbished for evaluation as part of studies into cruise missile development.[6]
A Grebe, in "Type IV" configuration, is on display at the United States Naval Undersea Museum in Keyport, Washington.[7]
. Norman Friedman. U.S. Naval Weapons: Every gun, missile, mine, and torpedo used by the U.S. Navy from 1883 to the present day. 1982. Naval Institute Press. Annapolis, MD. 978-0-87021-735-7.