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"Little Scraps Can Add Up to a Whale of a Lot; You may not be a little fish in a big pond, but you must do your part to safeguard classified materials. That minnow of information you inadvertently let loose may be the catch-of-the-day for some trolling listener. And, that's no fish story."
Whale eating scraps of paper with information on it in the ocean -
"Living in Huntsville and Madison County: Home of George C. Marshall Space Flight Center."
This pamphlet includes a memo to "Key MSFC Employees" from M. Keith Wible, Chief of the Manpower Utilization and Administration Office at Marshall Space Flight Center. -
"LM System Description."
Report that describes the major systems of the Lunar Module. -
"Loose chips sink ships, disable tanks, ground planes, etc., etc.; Careful what you put on the web."
Computer screen with puzzle pieces putting together the classified mission information -
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"Lunar Applications of a Spent S-IVB/IU stage (LASS)."
Support of lunar exploration missions is a major consideration in future space program planning. The spent Saturn v/S-IVB/IU can support both lunar - orbit and lunar -landing operations. This paper investigates lunar applications of the spent stage, and incorporates data generated during Company-funded studies. Investigated here is the feasibility of using a launch vehicle employing standard S-IC and S-I1 boost stages to deliver a modified S-IVB/IU and large discretionary payloads to a lunar orbit (LASSO) and/or the lunar surface (LASS). Operations in Earth orbit and direct-ascent trajectories are examined, and consideration is given to the use of the spent stage as a shelter in a manner similar to the presently planned Earth orbital workshop operations. Both the LASSO and LASS concepts are recommended for consideration in future lunar exploration plans. These concepts are capable of placing a gross wet weight of 101,400 lb in lunar orbit or landing 63,580 lb on the lunar surface respectively. The effective payload capability can be enhanced by proper integration of translunar mission subsystems with the subsystems required for lunar orbit or surface operations. The vehicles can be available within 3 years, with current-technology hardware sufficient for performing the missions described.; Douglas Paper No. 4256. -
"M-45 casting alloy : Gyro stabilizer support."
8 x 10 inch black and white photograph of a gyro stabilizing support. -
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