ST-124-M3 inertial platform (English Wikipedia)

Analysis of information sources in references of the Wikipedia article "ST-124-M3 inertial platform" in English language version.

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5nasa.gov

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5handle.net

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Bilstein 1980, pp. 243–253. Bilstein, Roger E. (1980). "8: From Checkout to Launch: The Quintessential Computer". Stages to Saturn: A Technological History of the Apollo/Saturn Launch Vehicles. NASA History Series. NASA. pp. 243–253. hdl:2060/19970009949. ISBN 0-16-048909-1. NASA SP-4206; 97N-15592.
Haeussermann 1970, p. 1. Haeussermann, Walter (July 1970). Description and Performance of the Saturn Launch Vehicle's Navigation, Guidance, and Control System (Report). NASA. hdl:2060/19700023342. NASA TN-D-5869; 70N-32653.
Thomason 1965, p. 53: "The sleeve, endplates, and cylinder were constructed of beryllium with machined tolerances of 20 micro inches in roundness and 20 micro inches/inch in squareness." Thomason, Herman E. (September 1965). General Description of the ST-124M Inertial Platform System (Report). NASA. hdl:2060/19650024833. NASA TN-D-2983; 65N-34434. This has clearer figures than most of the PDF documents about the IU, providing the best views of the insides of the gyros and gas bearings.
Haeussermann 1970, p. 20: Gas bearing air gap 0.0015–0.002 centimetres (0.000591–0.000787 inches; 591–787 microinches) Haeussermann, Walter (July 1970). Description and Performance of the Saturn Launch Vehicle's Navigation, Guidance, and Control System (Report). NASA. hdl:2060/19700023342. NASA TN-D-5869; 70N-32653.
Thomason 1965, p. 10. Thomason, Herman E. (September 1965). General Description of the ST-124M Inertial Platform System (Report). NASA. hdl:2060/19650024833. NASA TN-D-2983; 65N-34434. This has clearer figures than most of the PDF documents about the IU, providing the best views of the insides of the gyros and gas bearings.

nasa.gov

ntrs.nasa.gov

Bilstein 1980, pp. 243–253. Bilstein, Roger E. (1980). "8: From Checkout to Launch: The Quintessential Computer". Stages to Saturn: A Technological History of the Apollo/Saturn Launch Vehicles. NASA History Series. NASA. pp. 243–253. hdl:2060/19970009949. ISBN 0-16-048909-1. NASA SP-4206; 97N-15592.
Haeussermann 1970, p. 1. Haeussermann, Walter (July 1970). Description and Performance of the Saturn Launch Vehicle's Navigation, Guidance, and Control System (Report). NASA. hdl:2060/19700023342. NASA TN-D-5869; 70N-32653.
Thomason 1965, p. 53: "The sleeve, endplates, and cylinder were constructed of beryllium with machined tolerances of 20 micro inches in roundness and 20 micro inches/inch in squareness." Thomason, Herman E. (September 1965). General Description of the ST-124M Inertial Platform System (Report). NASA. hdl:2060/19650024833. NASA TN-D-2983; 65N-34434. This has clearer figures than most of the PDF documents about the IU, providing the best views of the insides of the gyros and gas bearings.
Haeussermann 1970, p. 20: Gas bearing air gap 0.0015–0.002 centimetres (0.000591–0.000787 inches; 591–787 microinches) Haeussermann, Walter (July 1970). Description and Performance of the Saturn Launch Vehicle's Navigation, Guidance, and Control System (Report). NASA. hdl:2060/19700023342. NASA TN-D-5869; 70N-32653.
Thomason 1965, p. 10. Thomason, Herman E. (September 1965). General Description of the ST-124M Inertial Platform System (Report). NASA. hdl:2060/19650024833. NASA TN-D-2983; 65N-34434. This has clearer figures than most of the PDF documents about the IU, providing the best views of the insides of the gyros and gas bearings.