The rubber nozzle is all cracked.

那只橡胶喷了。

It is shown that test aerospike nozzle has good altitude compensability of thrust.

实验表明，塞式喷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、喷堵片的设计方法进行了阐述。

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。

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。

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计为究,序列计、药量的估算、喷管堵片的计方法进行了阐述。

The rubber nozzle is all cracked.

那只橡胶管全裂了。

It is shown that test aerospike nozzle has good altitude compensability of thrust.

实验表，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.

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、管堵片的设计方法进行了阐述。

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.

以某型号发动机尾设计为究象,序列设计、药量的估算、喷管堵片的设计方法进行了阐述。

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，塞式喷管具有良好高度补和较高效率。

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计为究对象,对点火序列计、点火药量估算、喷管堵计方法进行了阐述。

The rubber nozzle is all cracked.

那只管全裂了。

It is shown that test aerospike nozzle has good altitude compensability of thrust.

实验表明，塞式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、管堵片的设计方法进行了阐述。

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,点火序列、点火药量的估算、喷管堵片的方法进行了阐述。

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。