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Hiroc
Part of Atlas
MX-774
MX-774
Credit: Ronald Wade
American test vehicle. Project MX-774 inaugurated by AAF with Consolidated-Vultee to study rocket capabilities with an ICBM as a final objective. Limited funds permitted a few test launches. These rockets demonstrated technologies that would later be applied to the Atlas.

AKA: MX-774;RTV-A-2;Upper Air Test Vehicle. Status: Cancelled 1947. First Launch: 1948-07-14. Last Launch: 1948-12-02. Number: 3 . Thrust: 35.00 kN (7,868 lbf). Gross mass: 1,300 kg (2,800 lb). Unfuelled mass: 700 kg (1,540 lb). Height: 9.60 m (31.40 ft). Diameter: 0.76 m (2.49 ft). Apogee: 50 km (31 mi).

In 1945 the U.S. Army Air Force awarded Consolidated-Vultee project MX-774, which was to lead to a long-range ballistic missile. The Air Force contracted for ten MX-774 vehicles, in three phases. Stage A, the Teetotaler, was a sub-sonic, self-guided cruise missile. Stage B, the Old Fashioned, was a test missile using V-2 technology but incorporating new concepts planned for the next phase. Stage C, the Manhattan, was to be an ICBM. The MX-774 was cancelled by the Air Force in June 1947 due to budget restrictions and continued Air Force skepticism. Using residual contract and corporate funds, Bossart was able to launch three stage B test vehicles from White Sands after the cancellation.

A Reaction Motors XLR35-RM-1 four-chamber liquid-propellant rocket motor was fitted to the rocket's cylindrical body. Four fixed stabilizing fins provided stability. New technologies demonstrated gimbaled rocket nozzles, a separable nose cone, and the balloon internal pressure stabilized flight structure. The missile's skin was very thin, and was inflated by internal pressure like a balloon. Three Hiroc's were flown in July to December 1948.

While none of the launches were completely successful, they did demonstrate Bossart's innovative design concepts including pressurized monocoque propellant tanks. Despite the heavy investment of company funds, the Air Force later directed Bossart to sell the MX-774 development package to TRW for a song. TRW in turn delivered it, in total, to Douglas and Martin to assist them in design of their competing Thor and Titan missiles. There were many hard feelings at Convair about that. However the know-how obtained in designing and building the Hiroc would be the starting point for their Atlas ICBM just a few years later.


More at: Hiroc.

Subtopics

Atlas The Atlas rocket, originally developed as America's first ICBM, was the basis for most early American space exploration and was that country's most successful medium-lift commercial launch vehicle. It launched America's first astronaut into orbit; the first generations of spy satellites; the first lunar orbiters and landers; the first probes to Venus, Mars, Mercury, Jupiter, and Saturn; and was America's most successful commercial launcher of communications satellites. Its innovative stage-and-a-half and 'balloon tank' design provided the best dry-mass fraction of any launch vehicle ever built. It was retired in 2004 after 576 launches in a 47-year career.

Family: test vehicle. Country: USA. Engines: LR35. Propellants: Lox/Alcohol. Launch Sites: White Sands LC33, White Sands. Agency: Convair.

1946 January 11 - . LV Family: Atlas. Launch Vehicle: Hiroc.
1946 April 2 - . LV Family: Atlas. Launch Vehicle: Hiroc.
1946 December - . LV Family: Atlas. Launch Vehicle: Hiroc.
Early 1947 - . LV Family: Atlas. Launch Vehicle: Hiroc.
1947 July 1 - . LV Family: Atlas. Launch Vehicle: Hiroc.
1947 October - . LV Family: Atlas. Launch Vehicle: Hiroc.
1947 November 20 - . LV Family: Atlas. Launch Vehicle: Hiroc.
1948 January - . LV Family: Atlas. Launch Vehicle: Hiroc.
1948 May 6 - . LV Family: Atlas. Launch Vehicle: Hiroc.
1948 June - . LV Family: Atlas. Launch Vehicle: Hiroc.
1948 July 14 - . 01:05 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: Atlas. Launch Vehicle: Hiroc. FAILURE: Cutoff after half of the propellants were used.. Failed Stage: 1.
1948 September 27 - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: Atlas. Launch Vehicle: Hiroc. FAILURE: Cutoff at 16 km altitude.. Failed Stage: 1.
1948 December 2 - . 22:01 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: Atlas. Launch Vehicle: Hiroc. FAILURE: Vibration closed valve early..
1949 February - . LV Family: Atlas. Launch Vehicle: Hiroc.
During 1949 - . LV Family: Atlas. Launch Vehicle: Hiroc.

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