Has use | Crewed expendable launch system |
---|---|
Manufacturer | Convair |
Country of origin | United States |
Size | |
Height | 28.7 metres (94.3 ft) |
Diameter | 3.0 metres (10.0 ft) width over boost fairing 4.9 metres (16 ft) |
Mass | 120,000 kilograms (260,000 lb) |
Stages | 1+1⁄2 |
Capacity | |
Payload to LEO | |
Mass | 1,360 kilograms (3,000 lb) [2] |
Launch history | |
Status | Retired |
Launch sites | CCAFS LC-14 |
Total launches | 9 |
Success(es) | 7 |
Failure(s) | 2 |
First flight | 29 July 1960 |
Last flight | 15 May 1963 |
Boosters | |
No. boosters | 1 |
Powered by | 2 Rocketdyne XLR-89-5 |
Maximum thrust | 1,517.4 kilonewtons (341,130 lbf) |
Burn time | 135 seconds |
Propellant | RP-1/LOX |
First stage | |
Diameter | 3.0 metres (10.0 ft) |
Powered by | 1 Rocketdyne XLR-105-5 |
Maximum thrust | 363.22 kilonewtons (81,655 lbf) |
Burn time | 5 minutes |
Propellant | RP-1/LOX |
The Atlas LV-3B ,Atlas D Mercury Launch Vehicle or Mercury-Atlas Launch Vehicle,was a human-rated expendable launch system used as part of the United States Project Mercury to send astronauts into low Earth orbit. Manufactured by American aircraft manufacturing company Convair,it was derived from the SM-65D Atlas missile,and was a member of the Atlas family of rockets. [3]
The Atlas D missile was the natural choice for Project Mercury since it was the only launch vehicle in the US arsenal that could put the spacecraft into orbit and also had many flights from which to gather data. But its reliability was far from perfect,and Atlas launches ending in explosions were an all-too common sight at Cape Canaveral. The Atlas had also been originally designed as a weapon system,thus its design and reliability did not need to necessarily be 100% perfect. As such,significant steps had to be taken to human-rate the missile and make it safe and reliable unless NASA wished to spend several years developing a dedicated launch vehicle for crewed programs or else wait for the next-generation Titan II ICBM to become operational. Atlas' stage-and-a-half configuration was seen as preferable to the two stage Titan in that all engines were ignited at liftoff,making it easier to test for hardware problems during pre-launch checks. [4]
Shortly after being chosen for the program in early 1959,the Mercury astronauts were taken to watch the second D-series Atlas test,which exploded a minute into launch. This was the fifth straight complete or partial Atlas failure and the booster was at this point nowhere near reliable enough to carry a nuclear warhead or an uncrewed satellite,let alone a human passenger. Plans to human-rate Atlas were effectively still on the drawing board and Convair estimated that 75% reliability would be achieved by early 1961 and 85% reliability by the end of the year. Despite the Atlas' developmental problems,NASA had the benefit of conducting Project Mercury simultaneously with the Atlas R&D program which gave plenty of test flights to draw data from as well as test modified equipment for Mercury. [3]
Flight | Crew member | Mission name | Date | Outcome |
---|---|---|---|---|
1 | Uncrewed | Mercury Atlas-3 | Tuesday,April 25,1961 11:15 AM EST [lower-alpha 2] [5] | Failure |
First flight of the Atlas LV-3B. Was an uncrewed test flight. Resulted in failure. The cause remains disputed. | ||||
2 | Uncrewed | Mercury Atlas-4 | Wednesday,September 13,1961 10:04 AM EDT [6] | Success |
Second uncrewed test flight. The launch was successful. | ||||
3 | Uncrewed | Mercury Atlas-5 | Wednesday Nov 29th,1961 10:07 AM EST [6] | Success |
Final uncrewed test flight. Launch was successful. | ||||
4 | John Glenn | Mercury Atlas-6 | Tuesday,February 20,1962 9:47 AM EST [7] | Success |
First crewed flight of the Atlas LV-3B. Successfully launched John Glenn to become the first American to orbit the Earth. First flight of John Glenn. | ||||
5 | Scott Carpenter [8] | Mercury Atlas-7 | Thursday,May 24,1962 8:45 AM EDT [7] | Success |
Second crewed flight of the Atlas LV-3B. First flight of Scott Carpenter. | ||||
6 | Wally Schirra [9] | Mercury Atlas-8 | Wednesday,October 3,1962 8:15 AM EDT [7] | Success |
Third crewed flight of the Atlas LV-3B. First flight of Wally Schirra. | ||||
7 | Gordon Cooper [10] | Mercury Atlas-9 | Wednesday,May 15,1963 9:04 AM EDT [7] | Success |
Final flight of the Atlas LV-3B. Final crewed flight of the Atlas LV-3B. First flight of Gordon Cooper. | ||||
8 | Alan Shepard | Mercury-Atlas 10 | October 1963 [11] | Cancelled |
Was to be second flight of Alan Shepard. Was to be final flight of the Atlas LV-3B. Was cancelled because it was determined to be too risky. [12] |
Project Mercury was the first human spaceflight program of the United States, running from 1958 through 1963. An early highlight of the Space Race, its goal was to put a man into Earth orbit and return him safely, ideally before the Soviet Union. Taken over from the US Air Force by the newly created civilian space agency NASA, it conducted 20 uncrewed developmental flights, and six successful flights by astronauts. The program, which took its name from Roman mythology, cost $2.27 billion. The astronauts were collectively known as the "Mercury Seven", and each spacecraft was given a name ending with a "7" by its pilot.
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. Atlas became operational in October 1959, but was soon made obsolete as an ICBM by new development, and was retired from this role by 1965.
Cape Canaveral Space Force Station (CCSFS) is an installation of the United States Space Force's Space Launch Delta 45, located on Cape Canaveral in Brevard County, Florida.
Gemini 1 was the first mission in NASA's Gemini program. An uncrewed test flight of the Gemini spacecraft, its main objectives were to test the structural integrity of the new spacecraft and modified Titan II launch vehicle. It was also the first test of the new tracking and communication systems for the Gemini program and provided training for the ground support crews for the first crewed missions.
Mercury-Atlas 1 (MA-1) was the first attempt to launch a Mercury capsule and occurred on July 29, 1960 at Cape Canaveral, Florida. The spacecraft was unmanned and carried no launch escape system. The Atlas rocket suffered a structural failure 58 seconds after launch at an altitude of approximately 30,000 feet (9.1 km) and 11,000 feet (3.4 km) down range. All telemetry signals suddenly ceased as the vehicle was passing through Max Q. Because the day was rainy and overcast, the booster was out of sight from 26 seconds after launch, and it was impossible to see what happened.
Mercury-Atlas 2 (MA-2) was an unmanned test flight of the Mercury program using the Atlas rocket. It launched on February 21, 1961 at 14:10 UTC, from Launch Complex 14 at Cape Canaveral, Florida.
Project Gemini was NASA's second human spaceflight program. Conducted between projects Mercury and Apollo, Gemini started in 1961 and concluded in 1966. The Gemini spacecraft carried a two-astronaut crew. Ten Gemini crews and 16 individual astronauts flew low Earth orbit (LEO) missions during 1965 and 1966.
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The Atlas-Centaur was a United States expendable launch vehicle derived from the SM-65 Atlas D missile. Launches were conducted from Launch Complex 36 at the Cape Canaveral Air Force Station (CCAFS) in Florida.
Launch Complex 14 (LC-14) is a launch site at Cape Canaveral Space Force Station in Florida. LC-14 was used for various manned and unmanned Atlas launches, including the February 1962, Friendship 7 flight aboard which John Glenn became the first American to orbit the Earth.
The Atlas-Agena 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 launched 109 times between 1960 and 1978. It was used to launch the first five Mariner uncrewed probes to the planets Venus and Mars, and the Ranger and Lunar Orbiter uncrewed probes to the Moon. The upper stage was also used as an uncrewed orbital target vehicle for the Gemini crewed spacecraft to practice rendezvous and docking. However, the launch vehicle family was originally developed for the Air Force and most of its launches were classified DoD payloads.
Atlas is a family of US missiles and space launch vehicles that originated with the SM-65 Atlas. The Atlas intercontinental ballistic missile (ICBM) program was initiated in the late 1950s under the Convair Division of General Dynamics. Atlas was a liquid propellant rocket burning RP-1 fuel with liquid oxygen in three engines configured in an unusual "stage-and-a-half" or "parallel staging" design: two outboard booster engines were jettisoned along with supporting structures during ascent, while the center sustainer engine, propellant tanks and other structural elements remained connected through propellant depletion and engine shutdown.
The SM-65D Atlas, or Atlas D, was the first operational version of the U.S. Atlas missile. Atlas D was first used as an intercontinental ballistic missile (ICBM) to deliver a nuclear weapon payload on a suborbital trajectory. It was later developed as a launch vehicle to carry a payload to low Earth orbit on its own, and later to geosynchronous orbit, to the Moon, Venus, or Mars with the Agena or Centaur upper stage.
The Mercury-Redstone Launch Vehicle, designed for NASA's Project Mercury, was the first American crewed space booster. It was used for six sub-orbital Mercury flights from 1960–1961; culminating with the launch of the first, and 11 weeks later, the second American in space. The four subsequent Mercury human spaceflights used the more powerful Atlas booster to enter low Earth orbit.
The Titan II GLV or Gemini-Titan II was an American expendable launch system derived from the Titan II missile, which was used to launch twelve Gemini missions for NASA between 1964 and 1966. Two uncrewed launches followed by ten crewed ones were conducted from Launch Complex 19 at the Cape Canaveral Air Force Station, starting with Gemini 1 on April 8, 1964.
The Atlas LV-3B, Atlas D Mercury Launch Vehicle or Mercury-Atlas Launch Vehicle, was a human-rated expendable launch system used as part of the United States Project Mercury to send astronauts into low Earth orbit. Manufactured by Convair, it was derived from the SM-65D Atlas missile, and was a member of the Atlas family of rockets. With the Atlas having been originally designed as a weapon system, testing and design changes were made to the missile to make it a safe and reliable launch vehicle. After the changes were made and approved to, the US launched the LV-3B nine times, four of which had crewed Mercury spacecraft.
The LR87 was an American liquid-propellant rocket engine used on the first stages of Titan intercontinental ballistic missiles and launch vehicles. Composed of twin motors with separate combustion chambers and turbopump machinery, it is considered a single unit. The LR87 first flew in 1959.
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