XSM-73 Goose

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XSM-73 Bull Goose
XSM-73 at Launch
TypeCruise Missile
Service history
In serviceCancelled
Production history
ManufacturerFairchild
Produced1957
Specifications
Mass8,945 lb (4,057 kg) including booster
Length33 ft 6 in (10.21 m)
Height7 ft 1 in (2.16 m)
Wingspan24 ft 5 in (7.44 m)
WarheadNone
PropellantThiokol solid-propellant rocket; 50,000 lbf (222 kN) thrust for 3 seconds.
Operational
range
4,773 mi (7,681 km)
Flight ceiling50,000 ft (15,200 m)
Flight altitude50,000 ft (15,200 m) at 3,701 lb (1,679 kg) at Mach 0.85
Maximum speed Mach 0.85
Guidance
system
Autopilot integrated with a rate integrating gyroscope pre-programmed to turn the SM-73.
Launch
platform
Zero-length ground launcher.
XSM-73 being prepared for flight.

The

B-52 bomber
on radar.

Development

Starting in December 1952, Fairchild began concept studies for a ground-launched long range decoy missile that could simulate strategic bombers on radar.[1]

In March 1953, the

air defense system.[1][2]
Multiple SM-73 missiles would be ground-launched from Strategic Air Command bases located in the continental United States. The requirement was that fifty percent of the deployed SM-73 missiles could be launched within the first hour after a launch order and the remaining missiles could be launched within one more hour.
B-52 Stratofortress over the final 1,500 nm (2,780 km) of flight.[3]

Study contracts were awarded to Convair and Fairchild in July 1954 by the United States Air Force under the project designation MX-2223.

The Fairchild MX-2223 design called for a non-metallic fuselage with swept wings and a v-tail. Radar reflectors were located in the fuselage and on pods positioned on the wing tips to simulate the radar return of a bomber.

Design

In December 1955, Fairchild was awarded a contract to develop Weapon System 123A which included the SM-73 missile. American Machine and Foundry Company was responsible for the ground equipment, Ramo-Woodridge Corporation was responsible for electronic equipment, and Paul Omohundro Co who was responsible for airframe elements.

Two engine contracts were awarded by the USAF in November 1954 to minimize development risk.[5]

Each engine was in the 2,450 lbf (10.9 kN) thrust class with a thrust to weight ratio goal of 10:1. General Electric was awarded a contract for the development of the General Electric J85 and Fairchild was awarded a contract for the a competing engine the Fairchild J83. Fairchild proposed a lightweight engine of conventional design.[5]

The proposed General Electric engine had a more advanced design, involving more risk, but having a higher thrust to weight ratio. The XSM-73 was powered by the Fairchild J83 on all test flights but was also capable of using the General Electric J85. The Fairchild J83 was operating by early 1957.[5]

Like the MX-2223 design, the SM-73 utilized a non-metallic fiberglass fuselage.

booster
was used to launch the SM-73 to a speed of 300 knots (345 mph).

Cruise speed for the SM-73 was 488 knots (562 mph). The SM-73 had a fuel capacity of 803 gal (3,040 L) of JP-4. This fuel was stored in 10 fuselage and six wing tanks.[3]

An

Yaw control was provided by a rudder.[3] The control system positioned flight controls by sending electrical signals to hydraulic actuators
located at each flight control.

The SM-73 was designed to carry radar reflectors and active

L-band, and lower frequencies.[3]
The SM-73 was not armed.

Funding issues and problems with the fiberglass wing, the booster rocket, and the Fairchild J83 engine delayed testing.[1]

SM-73 at the Hagerstown Aviation Museum

Test and evaluation began in February 1957 with

Patrick Air Force Base in June 1957. At Patrick Air Force Base, launch complexes 21[6] and 22[7] were constructed near the Cape Canaveral Light[6] to support SM-73 testing. Five dummy booster launches and fifteen test flights were flown between March 1957 and December 1958.[6]

The United States Air Force planned to purchase 2,328 operational missiles and 53 missiles for test and evaluation.

Ethan Allen Air Force Base, Vermont.[8] Construction of Bull Goose missile sites began in August 1958.[2]

In December 1958 the program was canceled because the missile was not able to simulate a B-52 on radar.

USD
.

The SD-5 Osprey reconnaissance drone was developed with the Goose as a basis.[9]

Variants

B-73
Original designation in Bomber sequence
XSM-73
Test and Evaluation prototypes.
SM-73
Production Missile designation.
Gander
Proposed surface-to-surface version capable of carrying a 1 Mt warhead 2,000 miles (3,200 km).[10]

Operator

Survivors

See also

Aircraft of comparable role, configuration, and era

Related lists

References

Citations

  1. ^ a b c d SM-73, Directory of U.S. Military Rockets and Missiles - Appendix 1: Early Missiles and Drones, by Andreas Parsch [1], retrieved November 10, 2007.
  2. ^ a b c d e f g h SM-73 Bull Goose, 1997 Web Page by the Federation of American Scientists, [2], retrieved November 10, 2007.
  3. ^ a b c d e f g Fairchild B-73 Bull Goose, Fact Sheet from the National Museum of the USAF, "Fact Sheets : Fairchild B-73 : Fairchild B-73". Archived from the original on August 6, 2009. Retrieved September 24, 2007., Retrieved on November 10, 2007.
  4. ^ Historical Essay by Andreas Parsch, Goose, "Archived copy". Archived from the original on October 19, 2007. Retrieved September 24, 2007.{{cite web}}: CS1 maint: archived copy as title (link), retrieved on November 10, 2007.
  5. ^ a b c d e The History of North American Small Gas Turbine Aircraft Engines, William Fleming and Richard Leyes, AIAA, 1999
  6. ^ a b c Encyclopedia Astronautica, Cape Canaveral LC21, "Archived copy". Archived from the original on July 6, 2008. Retrieved June 19, 2009.{{cite web}}: CS1 maint: archived copy as title (link) retrieved November 10, 2007.
  7. ^ Encyclopedia Astronautica, Cape Canaveral LC22, "Archived copy". Archived from the original on July 6, 2008. Retrieved June 19, 2009.{{cite web}}: CS1 maint: archived copy as title (link) retrieved November 10, 2007.
  8. ^ GOOSE (BULL GOOSE) Fact Sheet, Cliff Lethbridge, Spaceline Website, "Cape Canaveral Rocket and Missile Programs". Archived from the original on June 10, 2007. Retrieved September 24, 2007., retrieved November 10, 2007.
  9. ^ Newcome 2004, p.75.
  10. ^ "Surface-to-Surface: Aerodynamic Cruise". Flight. 74 (2602): 881. 5 December 1958.
  11. ^ List of Hagerstown Aviation Museum Aircraft, "Archived copy" (PDF). Archived from the original (PDF) on 2016-03-03. Retrieved 2017-01-23.{{cite web}}: CS1 maint: archived copy as title (link), retrieved November 10, 2007

Bibliography

Further reading

  • Bridgman, Leonard, ed. (1958). Jane's All the World's Aircraft 1958-59. London: Jane's All the World's Aircraft Publishing Co. Ltd. p. 303.
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