Atlas LV-3B

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Atlas LV-3B
Launch of Friendship 7 - GPN-2000-000686.jpg
An Atlas D LV-3B launching Mercury-Atlas 6
Function Manned 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
Capacity
Payload to LEO 1,360 kg[1]
Launch history
Status Retired
Launch sites CCAFS LC-14
Total launches 9
Successes 7
Failures 2
First flight 29 July 1960
Last flight 15 May 1963
Boosters ()
No boosters 1
Engines 2
Thrust 1,300 kilonewtons (300,000 lbf)
Burn time 134 seconds
Fuel RP-1/LOX
First Stage
Diameter 3.0 metres (10.0 ft)
Engines 1
Thrust 300 kilonewtons (67,000 lbf)
Burn time 5 minutes
Fuel RP-1/LOX

The Atlas LV-3B, Atlas D Mercury Launch Vehicle or Mercury-Atlas Launch Vehicle, was a man-rated expendable launch system used as part of the United States Project Mercury to send astronauts into low Earth orbit. It was derived from the SM-65D Atlas missile, and was a member of the Atlas family of rockets.

Nine LV-3Bs were launched, two on unmanned suborbital test flights, three on unmanned orbital test flights, and four with manned Mercury spacecraft.[2][full citation needed] Atlas LV-3B launches were conducted from Launch Complex 14 at Cape Canaveral Air Force Station, Florida.[2]

It first flew on 29 July 1960, conducting the suborbital Mercury-Atlas 1 test flight. The rocket suffered a structural failure shortly after launch, and as a result failed to place the spacecraft onto its intended trajectory.[citation needed] In addition to the maiden flight, the first orbital launch, Mercury-Atlas 3 also failed. This failure was due to a problem with the guidance system failing to execute pitch and roll commands, necessitating that the Range Safety Officer destroy the vehicle. The spacecraft separated by means of its launch escape system and was recovered 1.8 kilometres (1.1 mi) from the launch pad.

A further series of Mercury launches was planned, which would have used additional LV-3Bs; however these flights were canceled after the success of the initial Mercury missions.[citation needed] The last LV-3B launch was conducted on 15 May 1963, for the launch of Mercury-Atlas 9.

See also[edit]

References[edit]

  1. ^ Wade, Mark. "Atlas LV-3B / Mercury". Encyclopedia Astronautica. Retrieved 24 November 2011. 
  2. ^ a b Encyclopedia Astronautica - Atlas