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By Raymond L. Bisplinghoff, Holt Ashley, Robert L.Halfman

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Extra info for Aeroelasticity

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Rector MSC, at No',ember Control to 19-26, R. engine must pressure chamber be could pressure increased be from accomplished systems. November individual associated (;rumman 1964. subsystem was proposed December. be jointly 27, hardware Agreement test require- also reached to implement Cost reviewed and effort by MSC and 1965. q64"': "Staff the to increase for a chamber S. , feed during February Ill, Review Report, I'rogram which program and to studies could this reviewed development. revised thrust Attn: subcontractors Hardware Management GAEC, subsystem January W.

Apollo Spacecraft Flight Development Mission Program,” October 28, 1964. 26 At Langley Research Center, representatives from Langley, MSC, Ames Research Center, Avco Corporation, and North American met to discuss their independent conclusions of the data gathered from the Scout test of the Apollo heatshield material and to determine whether a second test was advisable. Langley’s report revealed that: the heatshield materials performed as predicted within the flight condition appropriate to Apollo; the Results of wind tunnel tests at Ames Research Center are shown in the accompanying four pictures.

MSC, protection meteoroid hazard. MSC, "AsPO Robert Apollo E. Smylie, space suit," MSC Vqeekly NAA, thermal garment. rules to determine garment 19-26 of the C. 5 and life support the 19-26 system and doffed and with kilonewtons of redesigning the of excess material for doffing donned condition 19-26 defined. protection in donning and pressurized total unit weight for the reliability design mobility per sq m ETG in the neck which restricted visibility. MSC, "ASI'O Francis 9-2820," Weekly J. DeVos, November Officials from container North would movable hard MSC, "ASPO MSC, to To ensure consistent that with packed Attn: November Systems and stowage stowage Weekly disposition," Crew American container NAA, Report, Chief, and be spacecraft's change Management MSC, to 19, 1964.

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