2003
DOI: 10.2963/jjtp.17.199
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Evaluation of Thermal Diffusivity of Rocket Nozzle Materials.

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Cited by 4 publications
(5 citation statements)
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“…Both phenolic resin and RF resin are flame resistant due to their molecular structure and thus can be used as heat-resistant/heat-shielding materials for space hardware applications. If the thermal capacity of RF resin is the same as that of phenolic resin 1.6 kJ kg –1 K –1 , then the thermal diffusivity of RB-3.6-2 was 0.9 m 2 s –1 . This value is close to that of heat-resistant cork-phenol resin composites and carbon composites used for rocket components. , By optimizing the molecular structure of the resin in the skeletal phase, it can be expected that these composite materials will be further improved in the future. Flame resistance was also investigated by applying a liquefied natural gas (LNG) burner flame at ∼1700 °C to the RF-boehmite nanofiber monolith (Figure , Movie, Supporting Information).…”
supporting
confidence: 66%
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“…Both phenolic resin and RF resin are flame resistant due to their molecular structure and thus can be used as heat-resistant/heat-shielding materials for space hardware applications. If the thermal capacity of RF resin is the same as that of phenolic resin 1.6 kJ kg –1 K –1 , then the thermal diffusivity of RB-3.6-2 was 0.9 m 2 s –1 . This value is close to that of heat-resistant cork-phenol resin composites and carbon composites used for rocket components. , By optimizing the molecular structure of the resin in the skeletal phase, it can be expected that these composite materials will be further improved in the future. Flame resistance was also investigated by applying a liquefied natural gas (LNG) burner flame at ∼1700 °C to the RF-boehmite nanofiber monolith (Figure , Movie, Supporting Information).…”
supporting
confidence: 66%
“…This value is close to that of heat-resistant cork-phenol resin composites and carbon composites used for rocket components. 31,32 By optimizing the molecular structure of the resin in the skeletal phase, it can be expected that these composite materials will be further improved in the future. Flame resistance was also investigated by applying a liquefied natural gas (LNG) burner flame at ∼1700 °C to the RF-boehmite nanofiber monolith (Figure 4, Movie, Supporting Information).…”
mentioning
confidence: 99%
“…The preform is carbonized in nitrogen atmosphere. The impregnation and carbonization are repeated to make the preform dense to bulk density of 1.60 g/cm 3 . The maximum temperature is 2000 °C on heat treatment.…”
Section: Methodsmentioning
confidence: 99%
“…Sato et al [3] use a laser flash method to measure the thermal diffusivity of three-dimensional woven C/C composite in the direction parallel to fiber. The laser flash method requires high power source to heat a sample instantaneously.…”
Section: Introductionmentioning
confidence: 99%
“…This value is close to that of heat resistant cork-phenol resin composites and carbon composites used for rocket components. [33][34] I anticipate further improving our materials by optimizing the molecular structure of the resin in the skeletal phase.…”
Section: Main Textmentioning
confidence: 99%