High Virgo
The High Virgo, also known as Weapons System 199C (WS-199C), was a prototype air-launched ballistic missile (ALBM) jointly developed by Lockheed and the Convair division of General Dynamics during the late 1950s. The missile proved moderately successful and aided in the development of the later GAM-87 Skybolt ALBM. It was also used in early tests of anti-satellite weapons.
Also recorded as Weapons System 199C · WS-199C
High Virgo
- Name
- High Virgo
- Field
- air-launched ballistic missile
- Period
- 1958
- Region
- United States
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Documentary summary
The High Virgo, also known as Weapons System 199C (WS-199C), was a prototype air-launched ballistic missile (ALBM) jointly developed by Lockheed and the Convair division of General Dynamics during the late 1950s. The missile proved moderately successful and aided in the development of the later GAM-87 Skybolt ALBM. It was also used in early tests of anti-satellite weapons.
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wikidata · Q5757365 · wikipedia · High Virgo
In this article
Key facts
Key facts
• Name — High Virgo • Origin — United States • Type — Air-launched ballistic missile • Is Missile — yes • Service — 1958–1959 • Used By — United States Air Force • Design Date — 1958 • Manufacturer — Lockheed Corporation • Number — 4 • Spec Label — WS-199C • Weight — 12000 lb • Length — 30 ft • Diameter — 31 in • Engine — Thiokol TX-20 • Engine Power — 222 kN • Vehicle Range — 185 mi • Speed — Mach 6 • Guidance — Inertial guidance • Propellant — Solid fuel • Ceiling — 250000 ft+ • Boost — 29 seconds • Launch Platform — Convair B-58 Hustler
Design and development
Design and development
As part of the WS-199 project to develop new strategic weapons for the United States Air Force's Strategic Air Command, the Lockheed Corporation and the Convair division of General Dynamics proposed the development of an air-launched ballistic missile, to be carried by the Convair B-58 Hustler supersonic medium bomber. In early 1958 the two companies were awarded a contract for development of the weapon, designated WS-199C and given the code-name "High Virgo". While the project was intended to be strictly a research-and-development exercise, it was planned that the weapon would be quickly capable of being developed into an operational system if required. The High Virgo missile was a single-stage weapon, powered by a solid-fueled Thiokol TX-20 rocket, and was equipped with an advanced inertial guidance system derived from that of the AGM-28 Hound Dog cruise missile. Four tailfins in a cruciform arrangement provided directional control. The missile was developed by Lockheed, utilising components developed for several existing missiles to reduce the cost of the project, and also to reduce the development time required. Convair was responsible for development of a pylon for carriage and launching of the missile from the prototype B-58, the pylon replacing the aircraft's normal weapons pod.
Operational history
Operational history
Four test flights of the High Virgo missile were conducted. Due to development problems, the first two did not include the inertial guidance system, instead they were fitted with a simple autopilot guiding the weapon on a pre-programmed course. Launched from its B-58 carrier aircraft at high altitude and supersonic speed, the initial flight, conducted on September 5, 1958, was a failure when the missile's controls malfunctioned. The second test, three months later, proved more successful, with the missile flying over a range of nearly 200 mi. The third flight test, the following June, utilized the inertial guidance system for the first time. It was a successful flight.
Anti-satellite test
Anti-satellite test
The fourth High Virgo missile was utilized in a test mission intended to demonstrate the capability of the missile for use as a "satellite interceptor", or anti-satellite missile (ASAT). The missile, modified with cameras to record the results of the test, was initially targeted at the Explorer 4 satellite. Due to errors in calculating the satellite's orbit Explorer 5 was targeted instead. The ASAT test mission, the final flight of the High Virgo missile, was conducted on September 22, 1959. Less than a minute after the launch of the missile from its B-58 carrier aircraft at Mach 2, the telemetry signal was lost. No data was recovered from the test, and the camera data, intended to be recovered afterward, was not located. Hence the test was inconclusive. No further test firings of High Virgo were conducted, the research project having been concluded. The Air Force had begun work on what would become the GAM-87 Skybolt missile, which incorporated lessons learned from the WS-199 project.
Launch history
Launch history
• Date/Time (GMT) — Launch site — Outcome — Remarks • | 1958-09-05 — AMR DZ — Apogee 13 km • | 1958-12-19 — AMR DZ — Apogee 76 km • | 1959-06-04 — AMR DZ — Apogee 51 km • | 1959-09-22 — AMR DZ — Inconclusive — Apogee 12 kmAltitude at which telemetry was lost. AMR DZ means Atlantic Missile Range Drop Zone.
Definition
Definition
The canonical record carries the following identifying particulars. It is also recorded that high Virgo is classified as an air-launched ballistic missile. It is also recorded that high Virgo is associated with United States. Institutional cataloguing adds that high Virgo is recorded from 1958.
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- United States
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Broader subject
1- air-launched ballistic missileTerminology
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The Encyclopedia exists whether or not anything is for sale. Corrections are recorded rather than overwritten, and every version of this record is kept. Published 14 August 2026.
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