Manufacturer | Convair Division of General Dynamics |
---|---|
Country of origin | United States |
Size | |
Height | 28 m (91 ft) |
Diameter | 3.05 m (10 ft) |
Payload to Trans-lunar injection | 170 kg (370 lb) |
Launch history | |
Status | Retired |
Launch sites | LC-12, 13 & 14, Cape Canaveral |
Total launches | 3 |
Failure(s) | 3 |
First flight | 26 November 1959 |
Last flight | 15 December 1960 |
The Atlas-Able was an American expendable launch system derived from the SM-65 Atlas missile. It was a member of the Atlas family of rockets, and was used to launch several Pioneer spacecraft towards the Moon. Of the five Atlas-Able rockets built, two failed during static firings, and the other three failed to reach orbit. [1]
The Atlas-Able was a three-and-a-half-stage rocket, with a stage-and-a-half Atlas missile as the first stage, an Able second stage, and an Altair third stage. [2]
The first Atlas-Able used an Atlas C as the first stage, [3] and was intended to carry Pioneer P-1, but exploded during a static fire test on 24 September 1959. [4]
The remaining Pioneer launches used Atlas D missiles. Launches were conducted from Launch Complexes 12 and 14 at the Cape Canaveral Air Force Station. One launch was planned from Launch Complex 13; this became the second Atlas-Able to be destroyed during a static firing, and hence never launched. [1]
Date | Serial No. | Mission | Launch Site | Outcome | Photo | |
---|---|---|---|---|---|---|
- | Atlas 9C | Pioneer P-1 | LC-14 | Failure. Explosion during a static fire test. | ||
26 November 1959 | Atlas 20D | Pioneer P-3 | LC-14 | Failure. The Payload fairing broke up at 45 seconds after liftoff, causing loss of the upper stage and payload. [6] | ||
25 September 1960 | Atlas 80D | Pioneer P-30 | LC-12 | Failure. A propellant feed on the second stage had a malfunction. [7] | ||
15 December 1960 | Atlas 91D | Pioneer P-31 | LC-12 | Failure. Vibration and/or debris from the Able adapter section ruptured the liquid oxygen tank of Atlas, causing an explosion. [8] |
Titan was a family of United States expendable rockets used between 1959 and 2005. The Titan I and Titan II were part of the US Air Force's intercontinental ballistic missile (ICBM) fleet until 1987. The space launch vehicle versions contributed the majority of the 368 Titan launches, including all the Project Gemini crewed flights of the mid-1960s. Titan vehicles were also used to lift US military payloads as well as civilian agency reconnaissance satellites and to send interplanetary scientific probes throughout the Solar System.
The SM-65 Atlas was the first operational intercontinental ballistic missile (ICBM) developed by the United States and the first member of the Atlas rocket family. It was built for the U.S. Air Force by the Convair Division of General Dynamics at an assembly plant located in Kearny Mesa, San Diego.
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Space Launch Complex 41 (SLC-41), previously Launch Complex 41 (LC-41), is an active launch site at Cape Canaveral Space Force Station. As of 2024, the site is used by United Launch Alliance (ULA) for Atlas V and Vulcan Centaur launches. Previously, it had been used by the United States Air Force for Titan IIIC, Titan IIIE, and Titan IV launches.
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