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Bold Orion
Bold Orion, with B-47 launch aircraft
TypeAir-launched ballistic missile
Place of originUnited States
Service history
In service1958–1959
Used byUnited States Air Force
Production history
Designed1958
ManufacturerMartin Aircraft
No. built12
Specifications (Two-stage version)
Length37 feet (11 m)
Diameter31 inches (0.79 m)

EngineFirst stage, Thiokol TX-20 Sergeant; 1,500 lbf (6.66 kN)
Second stage, ABL X-248 Altair; 2,800 lbf (12.45 kN)
PropellantSolid fuel
Operational
range
1,100 miles (1,800 km)
Launch
platform
B-47 Stratojet

The Bold Orion missile, also known as Weapons System 199B (WS-199B), was a prototype air-launched ballistic missile (ALBM) developed by Martin Aircraft during the 1950s. Developed in both one- and two-stage designs, the missile was moderately successful in testing, and helped pave the way for development of the GAM-87 Skybolt ALBM. In addition, the Bold Orion was used in early anti-satellite weapons testing, performing the first interception of a satellite by a missile.

Design and development[edit]

The Bold Orion missile was developed as part of Weapons System 199, initiated by the United States Air Force (USAF) in response to the U.S. Navy's Polaris program,[1] with funding authorised by the United States Congress in 1957.[2] The purpose of WS-199 was the development of technology that would be used in new strategic weapons for the USAF's Strategic Air Command, not to deliver operational weapons; a primary emphasis was on proving the feasibility of an air-launched ballistic missile.[2][3][4]

The designation WS-199B was assigned to the project that, under a contract awarded in 1958 to Martin Aircraft, would become the Bold Orion missile.[3] The design of Bold Orion was simple, using parts developed for other missile systems to reduce the cost and development time of the project.[3] The initial Bold Orion configuration was a single-stage vehicle, using a Thiokol TX-20 Sergeant solid-fuel rocket.[3][5] Following initial testing, the Bold Orion configuration was altered to become a two-stage vehicle, an Allegany Ballistics Laboratory Altair upper stage being added to the missile.[3][6]

Operational history[edit]

Having been given top priority by the Air Force,[7] the first flight test of the Bold Orion missile was conducted on May 26, 1958, from a Boeing B-47 Stratojet carrier aircraft,[3][8] which launched the Bold Orion vehicle at the apex of a high-speed, high-angle climb.[3][9] The zoom climb tactic, combined with the thrust from the rocket motor of the missile itself, allowed the missile to achieve its maximum range, or, alternatively, to reach space.[9]

A twelve-flight test series of the Bold Orion vehicle was conducted;[3]. Despite suffering only one outright failure, the initial flight tests of the single-stage rocket proved less successful than hoped.[3] Authorisation was received to modify the Bold Orion to become a two-stage vehicle. In addition to the modifications improving the missile's reliability, they increased the range of Bold Orion to over 1,000 miles (1,600 km).[4][10] Four of the final six test firings were of the two-stage vehicle. These were considered successful, and established that the ALBM was a viable weapon.[2][3]

ASAT test[edit]

The final test launch of Bold Orion, conducted on October 13, 1959, was a test of the vehicle's capabilities in the anti-satellite role.[11][12] Piloted by Carl E Brust Jr, the missile was launched from an altitude of 35,000 feet (11,000 m) from its B-47 mothership, the missile successfully intercepted the Explorer 6 satellite,[13] passing its target at a range of less than 4 miles (6.4 km) at an altitude of 156 miles (251 km).[14][3] If the missile had a nuclear warhead, the satellite would have been destroyed.[9][15]

The Bold Orion ASAT test was the first interception of a satellite by any method, proving that anti-satellite missiles were feasible.[11][16] This test, along with an earlier, unsuccessful test of the High Virgo missile in the anti-satellite role, had political repercussions. The Eisenhower administration sought to establish space as a neutral ground for everyone's use, and the "indication of hostile intent" given by the tests was frowned upon, with anti-satellite weapons development being soon curtailed.[9][17]

Legacy[edit]

The results of the Bold Orion project, along with those from the testing of the High Virgo missile, also developed under WS-199, provided data and knowledge that assisted the Air Force in forming the requirements for the follow-on WS-138A, which would produce the GAM-87 Skybolt missile.[3][18]

Launch history[edit]

Bold Orion on B-47 carrier aircraft
Date/Time (GMT) Rocket Launch site Outcome Remarks[19]
1958-05-26 Single-stage Cape Canaveral Success Apogee 8 km (5.0 mi)
1958-06-27 Single-stage Cape Canaveral Failure Apogee 12 km (7.5 mi)
1958-07-18 Single-stage Cape Canaveral Success Apogee 100 km (62 mi)
1958-09-25 Single-stage Cape Canaveral Success Apogee 100 km (62 mi)
1958-10-10 Single-stage Cape Canaveral Success Apogee 100 km (62 mi)
1958-11-17 Single-stage Cape Canaveral Success Apogee 100 km (62 mi)
1958-12-08 Two-stage Cape Canaveral Success Apogee 200 km (120 mi)
1958-12-16 Two-stage Cape Canaveral Success Apogee 200 km (120 mi)
1959-04-04 Two-stage AMR DZ Success Apogee 200 km (120 mi)
1959-06-08 Single-stage AMR DZ Success Apogee 100 km (62 mi)
1959-06-19 Single-stage Cape Canaveral Success Apogee 100 km (62 mi)
1959-10-13 Two-stage AMR DZ Success Apogee 200 km (120 mi)

AMR DZ means Atlantic Missile Range Drop Zone.

See also[edit]

Related development
Comparable weapons

References[edit]

Citations[edit]

  1. ^ Ball 1980, p.226.
  2. ^ a b c Yengst 2010, p.37.
  3. ^ a b c d e f g h i j k l Parsch 2005
  4. ^ a b Stares 1985, p.109.
  5. ^ Ordway and Wakeford 1960, p.30.
  6. ^ Smith 1981, p.178.
  7. ^ Missiles and Rockets, volume 5. Washington Countdown. p.9.
  8. ^ Friedman 2000, p.122.
  9. ^ a b c d Temple 2004, p.111.
  10. ^ Besserer and Besserer 1959, p.34.
  11. ^ a b Peebles 1997, p. 65.
  12. ^ Chronology 1961, p.89.
  13. ^ Bowman 1986, p.14.
  14. ^ Yenne 2005, p.67.
  15. ^ Bulkeley and Spinardi 1986, p.17.
  16. ^ Hays 2002, p.84.
  17. ^ Lewis and Lewis 1987, pp.93–95.
  18. ^ International Aeronautic Federation. Interavia volume 15, p.814.
  19. ^ Bold Orion Archived November 20, 2010, at the Wayback Machine. Encyclopedia Astronautica. Accessed 2011-01-19.

Bibliography[edit]

Further reading[edit]

External links[edit]