It is shown that test aerospike nozzle has good altitude compensability of thrust.
实验表明,塞式喷管具有良好的高度补偿能力和较高的效率。
It is shown that test aerospike nozzle has good altitude compensability of thrust.
实验表明,塞式喷管具有良好的高度补偿能力和较高的效率。
The rubber nozzle is all cracked.
那只橡胶喷管全裂了。
Taking aft-end igniter design for a rocket motor for example,design methods for ignition sequence,amorce quantity estimation and nozzle closure were described respectively.
号发动机尾部点
设计为
究对象,对点
序列设计、点
的估算、喷管堵片的设计方法进行了阐述。
声明:上例句、词性分类均由互联网资源自动生成,部分未经过人工审核,其表达内容亦不代表本软件的观点;若发现问题,欢迎向我们指正。
It is shown that test aerospike nozzle has good altitude compensability of thrust.
实验表明,塞式喷管具有良好的高度补偿能力和较高的效率。
The rubber nozzle is all cracked.
那只橡胶喷管全裂了。
Taking aft-end igniter design for a rocket motor for example,design methods for ignition sequence,amorce quantity estimation and nozzle closure were described respectively.
以某动机尾部
设
为
究对象,对
序列设
、
药量的估算、喷管堵片的设
方法进行了阐述。
声明:以上例句、词性分类均由互联网资源自动生成,部分未经过人工审核,其表达内容亦不代表本软件的观;若
现问题,欢迎向我们指正。
It is shown that test aerospike nozzle has good altitude compensability of thrust.
实验表明,塞式喷管具有高度补偿能力和较高
效率。
The rubber nozzle is all cracked.
那只橡胶喷管全裂了。
Taking aft-end igniter design for a rocket motor for example,design methods for ignition sequence,amorce quantity estimation and nozzle closure were described respectively.
以某型号发动机尾部点火设计为究对象,对点火序列设计、点火药量
估算、喷管堵片
设计方法进行了阐述。
声明:以上、词性分类均由互联网资源自动生成,部分未经过人工审核,其表达内容亦不代表本软件
观点;若发现问题,欢迎向我们指正。
It is shown that test aerospike nozzle has good altitude compensability of thrust.
实验表明,塞式喷管具有良好的高度补偿能力和较高的效率。
The rubber nozzle is all cracked.
那只橡胶喷管全裂了。
Taking aft-end igniter design for a rocket motor for example,design methods for ignition sequence,amorce quantity estimation and nozzle closure were described respectively.
以发动机尾部
设计为
究对象,对
序列设计、
量的估算、喷管堵片的设计方法进行了阐述。
声明:以上例句、词性分类均由互联网资源自动生成,部分未经过人工审核,其表达内容亦不代表本软件的观;若发现问题,欢迎向我们指正。
It is shown that test aerospike nozzle has good altitude compensability of thrust.
实验表明,塞式喷管具有高度补偿能力和较高
效率。
The rubber nozzle is all cracked.
那只橡胶喷管全裂了。
Taking aft-end igniter design for a rocket motor for example,design methods for ignition sequence,amorce quantity estimation and nozzle closure were described respectively.
以某型号发动机尾部点火设计为究对象,对点火序列设计、点火药量
估算、喷管堵片
设计方法进行了阐述。
声明:以上、词性分类均由互联网资源自动生成,部分未经过人工审核,其表达内容亦不代表本软件
观点;若发现问题,欢迎向我们指正。
It is shown that test aerospike nozzle has good altitude compensability of thrust.
验表明,塞式喷管具有良好的高度补偿能力和较高的效率。
The rubber nozzle is all cracked.
那只橡胶喷管全裂了。
Taking aft-end igniter design for a rocket motor for example,design methods for ignition sequence,amorce quantity estimation and nozzle closure were described respectively.
以某型号发机尾部点火设计为
究对象,对点火序列设计、点火药量的估算、喷管堵片的设计方法进行了阐述。
声明:以上例、词性分类均由互联网资
生成,部分未经过人工审核,其表达内容亦不代表本软件的观点;若发现问题,欢迎向我们指正。
It is shown that test aerospike nozzle has good altitude compensability of thrust.
实验表明,塞式喷管具有良好的高度补偿能力和较高的效率。
The rubber nozzle is all cracked.
那只橡胶喷管全裂了。
Taking aft-end igniter design for a rocket motor for example,design methods for ignition sequence,amorce quantity estimation and nozzle closure were described respectively.
以某型号发动机尾部计为
究
,
序列
计、
药量的估算、喷管堵片的
计方法进行了阐述。
声明:以上例句、词性分类均由互联网资源自动生成,部分未经过人工审核,其表达内容亦不代表本软件的观;若发现问题,欢迎向我们指正。
It is shown that test aerospike nozzle has good altitude compensability of thrust.
实验表明,塞式喷管具有高度补偿能力和较高
效率。
The rubber nozzle is all cracked.
那只橡胶喷管全裂了。
Taking aft-end igniter design for a rocket motor for example,design methods for ignition sequence,amorce quantity estimation and nozzle closure were described respectively.
以某型号发动机尾部点火设计为究对象,对点火序列设计、点火药量
估算、喷管堵片
设计方法进行了阐述。
声明:以上、词性分类均由互联网资源自动生成,部分未经过人工审核,其表达内容亦不代表本软件
观点;若发现问题,欢迎向我们指正。
It is shown that test aerospike nozzle has good altitude compensability of thrust.
实验表明,塞式喷管具有良好度补偿能力和较
率。
The rubber nozzle is all cracked.
那只橡胶喷管全裂了。
Taking aft-end igniter design for a rocket motor for example,design methods for ignition sequence,amorce quantity estimation and nozzle closure were described respectively.
以某型号发动机尾部点火设计为究对象,对点火序列设计、点火药量
估算、喷管堵片
设计
法
行了阐述。
声明:以上例句、词性分类均由互联网资源自动生成,部分未经过人工审核,其表达内容亦不代表本软件观点;若发现问题,欢迎向我们指正。