Prediction of nozzle material performance for NASA's 260 SL-3 motor.

Moody, Henry; Price, F. C.

doi:10.2514/3.29584

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A a Donskoy1

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“…'~ The same material was considered as one of the alternatives for rubber JBT-10, silicone-phenolic composition FM 5131, graphite-phenolic composition MX 4926 for heat shielding of the nozzle block of NASA 260 SL-3 type MESP. 35 A composition3' based on hydrocarbonic or acrylonitrile rubber containing a dehydrogenation component, a compound of the element of 4-6 period of the VIIIth group is described in Reference 36. The composition must not contain sulfur or sulfur containing compounds as vulcanizing agents to prevent the deterioration of its properties.…”

Section: A a Donskoymentioning

confidence: 99%