Saturn rocket testing (1 Ergebnisse)
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In den WarenkorbNASA materials engineering archive documenting cryogenic testing, fracture mechanics, and structural reliability research conducted during the development of the Saturn V launch vehicle and the Apollo spacecraft compiled at the George C. Marshall Space Flight Center. The materials originate from the Marshall Space Flight Center…during the 1960s when NASA engineers and contractors conducted intensive research on the mechanical behavior of rocket alloys exposed to extremely low temperatures and high stress conditions required for spaceflight. These studies formed part of the engineering foundation that enabled the Saturn V launch system used during the Apollo lunar missions. Comprising ten original reports and eight official NASA photographs of components and rocket design dated between 1961 and 1968, the collection documents low-temperature material testing and fracture resistance studies for launch vehicle components conducted by NASA engineers and contractors at the height of the U.S. space race. This archive originates from the estate of a decorated NASA materials engineer who began his career with the Guided Missile Development Division at Redstone Arsenal in 1951 and transitioned to NASA in 1960, working directly under Wernher von Braun. Serving as Deputy Chief of the Materials Division and later Assistant Director of the Materials and Processes Laboratory, he played a central role in early spacecraft development, receiving the NASA Exceptional Service Medal and the Yuri Gagarin Diploma. His work focused on cryogenic testing, low-temperature mechanical properties, and hydrogen embrittlement in metals-a crucial area for ensuring the performance and safety of rocket structures such as Saturn V and Apollo stages. the Apollo program extensively employed principles of fracture mechanics and materials testing to ensure the structural integrity of the spacecraft for all Apollo missions, including The moon landing with Apollo 11. The archive includes multiple internal notes and technical memoranda produced by the Propulsion and Vehicle Engineering Laboratory and the Metallic Materials Branch at Marshall Space Flight Center. NASA implemented fracture control requirements for human-rated spaceflight hardware to prevent catastrophic failures, even with potential flaws or cracks. Materials selection and testing: Engineers analyzed and tested various materials, These reports examine the cryogenic behavior and mechanical failure thresholds of specialized alloys used in rocket construction. Titles include: Low Temperature Mechanical Properties of Inconel 718 and AM 355 (Morgan, 1966) Low Temperature Mechanical Properties of High Strength A-286 Bolts (Menton) Low Temperature Mechanical Properties of Aluminum Alloy 2219-T87 (Denaburg, 1965) Low Temperature Mechanical Properties of 8Al-1Mo-1V Titanium Alloys and Composite Weldments (Denaburg, 1964) Low Temperature Thermal Expansion of Structural Metals (Miller & Buff, 1966) Mechanical Properties of 2219-T87 Alloy Plate at Room and Cryogenic Temperatures (Morgan, 1962) Reports contain detailed engineering summaries, including one stating: "The fully hardened (CSC 1000) AM 355 bar had satisfactory ultimate tensile and yield strengths at temperatures down to -423°F (4.2°K)." Another explains test methodology: "Determinations were made of the linear coefficient of thermal expansion. from 10° to 300°K with an accuracy of ±2.0 percent." Schematics of instrumentation appear in several volumes, including diagrams labeled "Interferometer-Dilatometer System and Dewar Assembly" and "Interferometer Telescope and Fringe Detecting Components." Visual material includes a large concept photo dated 1965 of a cutaway Saturn V rocket showing internal stage separation systems, propulsion chambers, and astronaut capsule modules. The reverse bears a stamp from the "Metallic Materials Branch, Metallurgical Analysis Section" and handwritten notation: "Photo Negative No. 65-1233." Also present are six original blac.
