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High Thermal Conductivity NARloy-Z-Diamond Composite for Advanced Rocket Engines.

机译：用于先进火箭发动机的高导热率NaRloy-Z-金刚石复合材料。

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作者
Bhat, B. N.; Greene, S.; Singh, J.; Ellis, D.;
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年度 2014
页码 1-10
总页数 10
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Composite materials; Diamonds; Thermal conductivity; Rocket engines; Nuclear propulsion; Temperature control; Combustion chambers; Management systems; Fabrication; Shapes; Linings;

机译：复合材料;钻石;导热系数;火箭发动机;核推进;温度控制;燃烧室;管理系统;制造;形状;衬里;

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1. Novel Functionalized BN Nanosheets/Epoxy Composites with Advanced Thermal Conductivity and Mechanical Properties [J] . Liu Zhan, Li Junhui, Liu Xiaohe ACS applied materials & interfaces . 2020,第5期

机译：新型官能化BN纳米片/环氧复合材料，具有先进的导热性和机械性能
2. Thermal conductivity of advanced TiC reinforced metal matrix composites for polymer processing applications [J] . Wilzer Jens, Windmann Matthias, Weber Sebastian, Journal of Composite Materials . 2015,第2期

机译：用于聚合物加工的高级TiC增强金属基复合材料的导热性
3. Epoxy nanocomposites with high thermal conductivity and low loss factor: Realize 3D thermal conductivity network at low content through core-shell structure and micro-nano technology [J] . Wang Rui, Xie Congzhen, Gou Bin, Polymer Testing . 2020,第1期

机译：具有高导热率和低损耗因子的环氧纳米复合材料：通过核心壳结构和微纳米技术实现低内容的3D导热网络
4. Fabrication of High Thermal Conductivity NARloy-Z-Diamond Composite Combustion Chamber Liner for Advanced Rocket Engines [C] . Biliyar N. Bhat, Sandra E. Greene, Jogender Singh AIAA/ASCE/AHS/ASC structures, structural dynamics and materials conference;AIAA SciTech Forum . 2016

机译：用于高级火箭发动机的高导热率NARloy-Z-金刚石复合燃烧室衬套的制造
5. Combustion and Magnetohydrodynamic Processes in Advanced Pulse Detonation Rocket Engines. [D] . Cole, Lord Kahil. 2012

机译：先进脉冲爆震火箭发动机的燃烧和磁流体动力学过程。
6. High-Thermal-Stability and High-Thermal-ConductivityTi3C2Tx MXene/Poly(vinylalcohol) (PVA) Composites [O] . Rui Liu, *, Weihua Li, 2018

机译：高热稳定性和高导热性Ti3C2Tx MXene /聚乙烯酒精）（PVA）复合材料
7. Novel Functionalized BN Nanosheets/Epoxy Composites with Advanced Thermal Conductivity and Mechanical Properties [O] . -1

机译：具有先进导热性和机械性能的新型官能化BN纳米片/环氧复合材料
8. Fabrication of High Thermal Conductivity NARloy-Z-Diamond Composite Combustion Chamber Liner for Advanced Rocket Engines. [R] . Bhat, B. N., Greene, S. E., Singh, J. 2016

机译：用于先进火箭发动机的高导热率NaRloy-Z-金刚石复合燃烧室内衬的制作。

High Thermal Conductivity NARloy-Z-Diamond Composite for Advanced Rocket Engines.

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