Technoarchaeology: Finding The Right Image in a Room Full of Tapes

Image: a portion of our set of Lunar Orbiter data tapes at McMoon’s – an abandoned McDonalds onsite at NASA Ames Research Park, home of the LOIRP – Lunar Orbiter Image recovery Project.
Here at the LOIRP (Lunar Orbiter Image Recovery Process) project there are two different phases of the image retrieval process that are distinct from each other. The second phase, the production of the vast majority of all the of the Lunar Orbiter images, will simply involve putting tapes on the tape drive machines, acquiring the data, and processing them into images.
However, we’re still in the first phase of the project where we need to search through tapes in a painstaking fashion just to find the images we are interested in downloading. Once we find what we are looking for, downloading is a snap and can be done in a matter of hours.
Finding the images using a jumbled nomenclature and labeling system last used more than 40 years ago is part of what we call “Technoarchaeology”.

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Correcting Our South Pole Selenography


“I have been involved in the illumination analysis of the lunar south pole for a while and your reference image (http://images.spaceref.com/news/2009/LO-IV-179-H1.label.jpg) seemed incorrect based on going over such images so many times.  I checked it against Clementine imagery and it turns out that the labels you have are in the wrong places.  I have attached a jpeg of the correct placements for the South Pole and Shackleton.” – James Fincannon, NASA GRC

LOIRP Releases Restored Image of Lunar South Pole

This image, LO-IV-179-H1, taken by Lunar Orbiter IV on May 24, 1967 at 16:19:23.809 GMT, shows a portion of the lunar south polar region. A much larger version [1.8 MB JPG] can be downloaded here. You can download the full resolution image [692 MB tiff] here at NLSI.
The altitude of the spacecraft when this image was taken was 3,591.83 kilometers. The resolution of the image is 78.432 meters per pixel.
Spacecraft Position: Altitude: 3591.83 km, Latitude: -71.38°, Longitude: -96.22°
Principal Point: Latitude: -69.52°, Longitude: -74.07°
Illumination: Sun Azimuth: 68.15°, Incident Angle: 82.85°, Emission Angle: 11.24°, Phase Angle: 94.08°, Alpha: -11.23°

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Lunar Orbiter IV Mission

Lunar Orbiter 4 was designed to take advantage of the fact that the three previous Lunar Orbiters had completed the required needs for Apollo mapping and site selection. It was given a more general objective, to “perform a broad systematic photographic survey of lunar surface features in order to increase the scientific knowledge of their nature, origin, and processes, and to serve as a basis for selecting sites for more detailed scientific study by subsequent orbital and landing missions”. It was also equipped to collect selenodetic, radiation intensity, and micrometeoroid impact data. The spacecraft was placed in a cislunar trajectory and injected into an elliptical near polar high lunar orbit for data acquisition. The orbit was 2,706 by 6,111 kilometres (1,681 3,797 mi) with an inclination of 85.5 degrees and a period of 12 hours.

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Lunar Orbiter 4 Mission

Alternate Names: Lunar Orbiter-D, 02772
Launch Date: 1967-05-04
Launch Vehicle: Atlas-Agena D
Launch Site: Cape Canaveral, United States
Mass: 385.6 kg
Nominal Power: 375.0 W
Launch/Orbital information for Lunar Orbiter 4
Experiments on Lunar Orbiter 4
Data collections from Lunar Orbiter 4
Description
Lunar Orbiter 4 was designed to take advantage of the fact that the three previous Lunar Orbiters had completed the required needs for Apollo mapping and site selection. It was given a more general objective, to “perform a broad systematic photographic survey of lunar surface features in order to increase the scientific knowledge of their nature, origin, and processes, and to serve as a basis for selecting sites for more detailed scientific study by subsequent orbital and landing missions. It was also equipped to collect selenodetic, radiation intensity, and micrometeoroid impact data. The spacecraft was placed in a cislunar trajectory and injected into an elliptical near polar high lunar orbit for data acquisition. The orbit was 2706 km x 6111 km with an inclination of 85.5 degrees and a period of 12 hours.

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