solid propellant

基本解釋

A non-flying prototype was intended to demonstrate that controlling unruly solid propellant would be possible during landing.
一個(gè)無(wú)法飛行的雛形預(yù)計(jì)將會(huì)演示，在著陸期間控制難以駕馭的固體推進(jìn)劑也是可能的。
Russian sources said that much more experimental work and funding would be required to prove that solid propellant could be safely used for a manned landing.
俄羅斯的消息人士稱，這將需要更多的試驗(yàn)工作以及資金來(lái)證明固體推進(jìn)劑可以被安全地用于載人著陸。
Solid-fuel rockets, in which the fuel and oxidiser are pre-mixed into a stable, solid propellant and then packed inside the case of the rocket, are simpler, lighter and relatively safer.
固體燃料火箭發(fā)動(dòng)機(jī)的構(gòu)造更簡(jiǎn)單、分量更輕，而且相對(duì)更安全。在固體燃料火箭發(fā)動(dòng)機(jī)里，燃料和氧化劑被預(yù)先混合成穩(wěn)定的液態(tài)推進(jìn)劑，然后被塞滿火箭發(fā)動(dòng)機(jī)的燃料箱里。

固體推進(jìn)劑
A moving solid propellant aircraft always gives out an apparent plume. The plume is an important target of attacking and early warning.
固體推進(jìn)劑飛行器在運(yùn)動(dòng)過(guò)程中往往產(chǎn)生明顯的尾焰羽煙,它不僅是全向攻擊的主要目標(biāo),也是早期預(yù)警的重要對(duì)象。
機(jī)械工程
固體推進(jìn)劑

固體火藥
The Non-Fourier conduction heat transfer model is developed on conventional ignition theory for solid propellant. The analytical and numerical solutions are obtained for a cylinder solid propellant grain.
結(jié)果表明,用非傅立葉導(dǎo)熱模型作為固體火藥點(diǎn)火理論的本構(gòu)關(guān)系,比傳統(tǒng)的火藥點(diǎn)火理論更能夠真實(shí)地反映等離子體與火藥的相互作用。
固體火箭推進(jìn)劑