打谷工具 发表于 2025-3-26 23:57:13

Efficiency Studies 2: Applications to Chinaproperties of the burning propellant surface layer, which in turn depend on the properties of the propellant components. The importance of formation of a surface layer and the properties of such structures as a skeleton layer is underlined. The results of these research activities open the possibili

Jogging 发表于 2025-3-27 05:02:19

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cumber 发表于 2025-3-27 08:41:54

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opprobrious 发表于 2025-3-27 11:40:33

Book 2017or access to, and exploration of, space..It will be of interest to both postgraduate and final-year undergraduate students in aerospace engineering, and practicing aeronautical engineers and designers, especially those with an interest in propulsion, as well as researchers in energetic materials..

mortuary 发表于 2025-3-27 14:45:27

1869-1730 inal-year undergraduate students in aerospace engineering, and practicing aeronautical engineers and designers, especially those with an interest in propulsion, as well as researchers in energetic materials..978-3-319-80207-7978-3-319-27748-6Series ISSN 1869-1730 Series E-ISSN 1869-1749

Favorable 发表于 2025-3-27 17:53:53

An Introduction to Energetic Materials for Propulsionin use today or in the near future. For every chapter, a short introduction is given of each included paper in order to help the reader to identify the contributions most suitable for their specific needs or interests. The final book chapter is dedicated to an historical survey of the Russian develo

过度 发表于 2025-3-27 22:07:40

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RACE 发表于 2025-3-28 03:04:25

High-Nitrogen Energetic Materials of 1,2,4,5-Tetrazine Family: Thermal and Combustion Behaviorstermine the condensed-phase combustion mechanism. The lack or low content of oxygen in tetrazine-based energetic materials results in formation of high-enthalpy species among combustion products, thus preventing from full release of energy stored in the material.

arterioles 发表于 2025-3-28 06:49:50

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短程旅游 发表于 2025-3-28 12:14:14

Introducing Tetrazole Salts as Energetic Ingredients for Rocket PropulsionO exhibits excellent thermal stability (the decomposition temperature is 230.3 °C, and the volume of the released gas is 0.30 mL·g. at 100 °C for 48 h) and low mechanical sensitivities (the explosion probabilities of impact sensitivity and friction sensitivity are 16 % and 24 %, respectively). The c
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查看完整版本: Titlebook: Chemical Rocket Propulsion; A Comprehensive Surv Luigi T. De Luca,Toru Shimada,Max Calabro Book 2017 Springer International Publishing Swit