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NASAs pre-Apollo program underwent a number of changes as the need to reach the moon before the Russians came to dominate the program.
One concept, that was studied and not proceeded with was mounting a small (100lb) rover to a modified Surveyor. It was to be fitted with small scientific package including a television camera (also used for navigation) and a penetrometer. Power was to come from an RTG.
It was intended to survey a potential Apollo landing site and one option considered was to fit it with a means of marking the landing point.
See:
1. Surveyor Lunar Roving Vehicle, Final Report, Vol. 1, Summary Report
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19660015678_1966015678.pdf
2. Surveyor Lunar Roving Vehicle, Final Report, Vol. 2, Mission and System Studies
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19660014483_1966014483.pdf
3. Surveyor Lunar Roving Vehicle, Final Report, Vol. 3, Preliminary System Description, Book 1, System Description
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19660004186_1966004186.pdf
4. Surveyor Lunar Roving Vehicle, Final Report, Vol. 3, Preliminary System Description, Book 2, Validation of Preliminary Design
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19660006194_1966006194.pdf
5. Surveyor Lunar Roving Vehicle, Final Report, Vol. 4, Reliability
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19660006188_1966006188.pdf
6. Surveyor Lunar Roving Vehicle, Final Report, Vol. 5, System Evaluation
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19660004162_1966004162.pdf
7. Interim Study for a Surveyor Lunar Roving Vehicle, Final Technical Report
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19660008345_1966008345.pdf
One concept, that was studied and not proceeded with was mounting a small (100lb) rover to a modified Surveyor. It was to be fitted with small scientific package including a television camera (also used for navigation) and a penetrometer. Power was to come from an RTG.
It was intended to survey a potential Apollo landing site and one option considered was to fit it with a means of marking the landing point.
See:
1. Surveyor Lunar Roving Vehicle, Final Report, Vol. 1, Summary Report
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19660015678_1966015678.pdf
2. Surveyor Lunar Roving Vehicle, Final Report, Vol. 2, Mission and System Studies
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19660014483_1966014483.pdf
3. Surveyor Lunar Roving Vehicle, Final Report, Vol. 3, Preliminary System Description, Book 1, System Description
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19660004186_1966004186.pdf
4. Surveyor Lunar Roving Vehicle, Final Report, Vol. 3, Preliminary System Description, Book 2, Validation of Preliminary Design
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19660006194_1966006194.pdf
5. Surveyor Lunar Roving Vehicle, Final Report, Vol. 4, Reliability
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19660006188_1966006188.pdf
6. Surveyor Lunar Roving Vehicle, Final Report, Vol. 5, System Evaluation
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19660004162_1966004162.pdf
7. Interim Study for a Surveyor Lunar Roving Vehicle, Final Technical Report
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19660008345_1966008345.pdf