|Table of Contents|

Analysis on test data of gelled propellant(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2008年01期
Page:
26-29
Research Field:
研究与设计
Publishing date:

Info

Title:
Analysis on test data of gelled propellant
Author(s):
Dou Shuangqing
Xi'all Aerospace Propulsion Test Technique Institute,Xi'an 710100,China
Keywords:
gelled pwpellantliquid flow testdata analysis
PACS:
V434
DOI:
-
Abstract:
Throush the theoretical analysis of non—Newtonian fluid.it is concluded that tIle flow characteristic of gelled propellant in the pipeline mainly depending on its own characteristics.There exists distinct difference between the calculation method of the pressure loss of gelled propellant and that of liquid propellant.This paper adopts the Allometric,polynomial and linear equations to perform the curve fitting and comparative analysis on the pressure versus flux test data of gelled N204 and UDMH,which reflects the non-Newtonian fluid characteristic of gelled propellant.Some suggestions to establish a system have been put forward.It is proposed that real medium should be used to carry out the cold conditioning prior to the test of gel test system.The feasible fitting method is also provided for system adjustment data in this paper.

References:

[l]代玉东.凝胶推进剂及其剂的制备和特性表征[J].火箭 推进.2004,30(4):59-64.
[2]杨伟东,张蒙正.凝胶推进剂流变及雾化特性研究与进 展[J].火箭推进.2005,3l(5):37—42.
[3]杨伟东,张蒙正.凝胶推进剂模拟液直圆管流动特性初 步研究[J].火箭推进.2006.32(3):12-18.
[4]符全军,杜宗罡,兰海平,等.UDMH/NTO双组元凝胶 推进剂的制备及性能研究[J].火箭推进,2006,32(1): 48-53.
[5]梁小强.凝胶试验系统的设计及试后处理工艺[J].火箭 推进,2006,32(4):51—53.
[6]江体乾.华工流变学[M].上海:华东理工大学出版社. 2004.
[7]李韵琳,徐温干,鲍金燕.凝胶推进剂及其在火箭发动 机上的应用[R].HQ-95017.
[8]张惠军.科氏力质量流量计在凝胶推进剂火箭发动机 试车中的应用[J].火箭推进.2004,30(6):55-60.

Memo

Memo:
-
Last Update: 1900-01-01