| XSSM-A-5 Boojum | |
|---|---|
.png) The final design of the XSSM-A-5 | |
| Type | Cruise missile |
| Place of origin | United States |
| Service history | |
| Used by | United States Air Force |
| Production history | |
| Designed | 1946–1951 |
| Manufacturer | Northrop Corporation |
| No. built | 0 |
| Specifications | |
| Mass | 112,000 pounds (51,000 kg) |
| Length | 85 feet 4 inches (26.01 m) |
| Height | 14 feet 9 inches (4.50 m) |
| Wingspan | 50 feet 10 inches (15.49 m) |
| Warhead | Nuclear |
| Engine | TwoJ47turbojets |
Operational range | 3,153 mi (5,075 km) |
| Flight ceiling | 70,000 feet (21,000 m) |
| Maximum speed | Mach 2 |
Guidance system | Celestial navigation |
TheXSSM-A-5 Boojum, also known by the project numberMX-775B, was a supersoniccruise missile developed by theNorthrop Corporation for theUnited States Air Force in the late 1940s. Intended to deliver anuclear warhead over intercontinental range, the project was determined to be too ambitious given technical difficulties with theSM-62 Snark which it was planned to follow, and it was canceled in 1951.
As part of aUnited States Army Air Forces effort to develop guided missiles for the delivery of nuclear weapons, the Northrop Corporation was awarded a development contract in March 1946 for the design of two long-range cruise missiles designated MX-775. The contract called for asubsonic missile MX-775A, later designatedSSM-A-3 Snark, and a more advancedsupersonic missile MX-775B, which in 1947 was given the name SSM-A-5 Boojum.[1] Northrop named the missiles after characters from the works ofLewis Carroll, withBoojum coming from the final line ofThe Hunting of the Snark.[2]
Designated N-25B by the company, the final design called for a long, slender missile, fitted withdelta wings, and powered by a pair ofGeneral Electricturbojet engines, mounted innacelles near the tips of the wing.[1][N 1]
The missile was intended to be launched using arocket sled; air-launch from aConvair B-36 heavy bomber was an alternative that was studied.[1] The missile would climb at subsonic speed to its operating altitude, then conduct a supersonic dash to the target area, guided by acelestial navigation system.[1] A "slipper" typedrop tank would be jettisoned halfway through the flight.[3] The Boojum was intended carry a warhead weighing up to 5,000 pounds (2,300 kg) over a range between 1,500 to 5,000 miles (2,400 to 8,000 km).[4]
At the end of 1946, the contracts that had been awarded to Northrop were revised; the Snark was canceled, while the Boojum was to be fully developed as an operational system.[5] Northrop lobbied for the reinstatement of the Snark, however; this was successful in getting the program reauthorized during 1947, with the Boojum being deferred to a follow-on project.[5]
Despite the design having been finalized, theUnited States Air Force (which the USAAF had become in 1948) determined that the project was technologically unfeasible, given continuing development difficulties and technical problems encountered during the Snark's development. Accordingly, in 1951, the Boojum project was canceled, before any prototypes of the missile had been constructed.[1][4]