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RTV-A-2 Hiroc

Spacecraft and Launch Vehicles

The RTV-A-2 Hiroc, short for high-altitude rocket, was a research rocket that Convair flew in 1947 at White Sands Proving Ground. It came out of the MX-774 project, the first United States effort to develop an intercontinental ballistic missile, which the Army cancelled in 1947; Convair used leftover funds to build and launch three of the planned ten research vehicles. The rocket was 9.6 m long and 760 mm in diameter, with an empty weight of 547 kg including payload and a gross liftoff weight of 1,860 kg, and it burned liquid oxygen and alcohol in an XLR35-RM-1 engine with four gimballed thrust chambers. All three flights, on 13 July, 27 September and 2 December 1947, partly failed through premature closure of the liquid oxygen valve, yet they proved gimballed engine guidance, a pressure-supported airframe and a separable nose cone, concepts later used on the Atlas missile.

Facts
Year
1947 1
Engine Class
Rocket 1
Status
Cancelled 1
Units Built
3 1
Mass (kg)
547 1
Maximum Mass (kg)
1860 1
Engine
XLR35-RM-1 1
Connections

Exemplifies

Source RTV-A-2 Hiroc (Wikipedia)

Of Make

Source RTV-A-2 Hiroc (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Encyclopedia Astronautica: HirocRelated, Agency
Quote, Related, Agency
Agency Convair

Originated In

Also in Geography Atlas: where this subject originated.

Source RTV-A-2 Hiroc (Wikipedia)Lead, country of origin
Quote, Lead, country of origin
was a product of the United States' first effort to develop an intercontinental ballistic missile
Sources
1. RTV-A-2 Hiroc (Wikipedia)
  • History
    The three tests took place on 13 July 1947, 27 September, and 2 December.
  • Lead
    The project was canceled in 1947, but leftover funds were used to build and launch three of the planned 10 research vehicles designated RTV-A-2.
  • Lead, engine class
    The RTV-A-2 Hiroc (high-altitude rocket)
  • Lead, units built
    leftover funds were used to build and launch three of the planned 10 research vehicles designated RTV-A-2
  • Design
    an empty weight including payload of 1,205 pounds (547 kg)
  • Design, maximum mass
    a gross liftoff weight (GLOW) of 4,090 pounds (1,860 kg)
  • Design, engine
    The missile's propulsion system consisted of an XLR35-RM-1 composed of four thrust chambers
  • History, manufacturer
    Convair arranged to use the remaining contract funding to launch three of the rockets, which were named RTV-A-2 Hiroc.
  • Lead, country of origin
    was a product of the United States' first effort to develop an intercontinental ballistic missile
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