The rubber nozzle is all cracked.
那只橡胶喷管全裂了。
The rubber nozzle is all cracked.
那只橡胶喷管全裂了。
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能力和较高的效率。
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为
究对象,对点火序列
、点火药量的估算、喷管堵片的
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点;若发现问题,欢迎向我们指正。
The rubber nozzle is all cracked.
那只橡胶喷管全裂了。
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。
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、词性类均由互联网资源自动生成,部
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。
The rubber nozzle is all cracked.
那只橡胶喷管全裂了。
It is shown that test aerospike nozzle has good altitude compensability of thrust.
明,塞式喷管具有良好的高度补偿能力和较高的效率。
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、点火药量的估算、喷管堵片的设计方法进行了阐述。
声明:以上例、词
分类均由互联网资源自动生成,部分未经过人工审核,其
达内容亦不代
本软件的观点;若发现问题,欢迎向我们指正。
The rubber nozzle is all cracked.
那只橡胶喷管全裂了。
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。
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:以上例句、词性类均由互联网资源自动生成,
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。
The rubber nozzle is all cracked.
那只橡胶全裂了。
It is shown that test aerospike nozzle has good altitude compensability of thrust.
实验表明,塞式具有良好的
度补偿能力
的效率。
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、点火药量的估算、
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点;若发现问题,欢迎向我们指正。
The rubber nozzle is all cracked.
那只橡胶喷管全裂了。
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。
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、词性分类均由互联网资源
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。
The rubber nozzle is all cracked.
那只橡胶喷管全裂了。
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。
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、词性类均由互联网资源自动生成,部
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。
The rubber nozzle is all cracked.
那只橡全裂了。
It is shown that test aerospike nozzle has good altitude compensability of thrust.
实验表明,塞式具有良好的高度补偿能力和较高的效率。
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、点火药量的估算、
堵片的设计方法进行了阐述。
声明:以上例句、词性分类均网资源自动生成,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。
The rubber nozzle is all cracked.
那只橡胶喷管全裂了。
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。
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:以上例句、词性类均由互联网资源自动生
,
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。
The rubber nozzle is all cracked.
橡胶喷管全裂了。
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。
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。