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Lunar Roving Vehicle Deploym
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| Name of Image |
Lunar Roving Vehicle Deployment Test |
| Date of Image |
1971-11-01 |
| Full Description |
This photograph shows workmen at the Boeing plant in Kent, Washington, performing deployment tests on the Lunar Roving Vehicle (LRV). The LRV, developed under the direction of the Marshall Space Flight Center, was designed to allow Apollo astronauts a greater range of mobility on the lunar surface during the last three lunar exploration missions, Apollo 15, Apollo 16, and Apollo 17. |
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Lunar Roving Vehicle Initial
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| Name of Image |
Lunar Roving Vehicle Initial Deployment Sequence |
| Date of Image |
1971-01-01 |
| Full Description |
This artist's concept illustrates the deployment sequence of the Lunar Roving Vehicle (LRV) on the Moon. The LRV was designed to transport astronauts and materials on the Moon. It was a collapsible open-space vehicle about 10 feet long with large mesh wheels, anterna, appendages, tool caddies, and cameras. Powered by two 36-volt batteries, it has four 1/4-hp drive motors, one for each wheel. The vehicle was designed to travel in forward or reverse, negotiate obstacles about 1 foot high, cross crevasses about 2 feet wide, and climb or descend moderate slopes. Its speed limit was about 9 miles (14 kilometers) per hour. An LRV was used on each of the last three Apollo missions (Apollo 15, Apollo 16, and Apollo 17) and permitted the crew to travel several miles from the Lunar Module. The LRV was designed, developed, and tested by the Marshall Space Flight Center, and built by the Boeing Plant in Kent, Washington. |
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Lunar Roving Vehicle (LRV) F
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| Name of Image |
Lunar Roving Vehicle (LRV) Flight Unit No. 1 |
| Date of Image |
1971-01-01 |
| Full Description |
The Lunar Roving Vehicle (LRV) was designed to transport astronauts and materials on the Moon. It was a collapsible open-space vehicle about 10 feet long with large mesh wheels, anterna, appendages, tool caddies, and cameras. Powered by two 36-volt batteries, it has four 1/4-hp drive motors, one for each wheel. The vehicle was designed to travel in forward or reverse, negotiate obstacles about 1 foot high, cross crevasses about 2 feet wide, and climb or descend moderate slopes. Its speed limit was about 9 miles (14 kilometers) per hour. An LRV was used on each of the last three Apollo missions (Apollo 15, Apollo 16, and Apollo 17) and permitted the crews to travel several miles from the Lunar Module. The LRV was designed, developed, and tested by the Marshall Space Flight Center, and built by the Boeing Plant in Kent, Washington. |
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Lunar Roving Vehicle (LRV) F
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| Name of Image |
Lunar Roving Vehicle (LRV) Flight Unit No. 2 |
| Date of Image |
1971-01-01 |
| Full Description |
The Lunar Roving Vehicle (LRV) was designed to transport astronauts and materials on the Moon. It was a collapsible open-space vehicle about 10 feet long with large mesh wheels, anterna, appendages, tool caddies, and cameras. Powered by two 36-volt batteries, it has four 1/4-hp drive motors, one for each wheel. The vehicle was designed to travel in forward or reverse, negotiate obstacles about 1 foot high, cross crevasses about 2 feet wide, and climb or descend moderate slopes. Its speed limit was about 9 miles (14 kilometers) per hour. An LRV was used on each of the last three Apollo missions (Apollo 15, Apollo 16, and Apollo 17) and permitted the crew to travel several miles from the Lunar Module. The LRV was designed, developed, and tested by the Marshall Space Flight Center, and built by the Boeing Plant in Kent, Washington. |
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Lunar Roving Vehicle Initial
…
| Name of Image |
Lunar Roving Vehicle Initial Deployment Sequence |
| Date of Image |
1971-01-01 |
| Full Description |
This artist's concept illustrates the deployment sequence of the Lunar Roving Vehicle (LRV) on the Moon. The LRV was designed to transport astronauts and materials on the Moon. It was a collapsible open-space vehicle about 10 feet long with large mesh wheels, anterna, appendages, tool caddies, and cameras. Powered by two 36-volt batteries, it has four 1/4-hp drive motors, one for each wheel. The vehicle was designed to travel in forward or reverse, negotiate obstacles about 1 foot high, cross crevasses about 2 feet wide, and climb or descend moderate slopes. Its speed limit was about 9 miles (14 kilometers) per hour. An LRV was used on each of the last three Apollo missions (Apollo 15, Apollo 16, and Apollo 17) and permitted the crew to travel several miles from the Lunar Module. The LRV was designed, developed, and tested by the Marshall Space Flight Center, and built by the Boeing Plant in Kent, Washington. |
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