冲压动力远程导弹燃料及起飞质量快速估算

doi:10.3969/j.issn.1009-086x.2018.01.008

现代防御技术 ›› 2018, Vol. 46 ›› Issue (1): 47-55.DOI: 10.3969/j.issn.1009-086x.2018.01.008

冲压动力远程导弹燃料及起飞质量快速估算

王宏涛, 石德平

中国航天科工集团有限公司第二研究院,北京 100854

收稿日期:2017-07-18 修回日期:2017-08-14 出版日期:2018-02-28 发布日期:2020-11-25
作者简介:王宏涛(1990-),男,北京人。博士生,主要从事飞行器总体设计研究。通信地址:100854 北京142信箱30分箱 E-mail:381094332@qq.com

Evaluation of Fuel and Take-off Mass for Tactical Scramjet Missile

WANG Hong-tao, SHI De-ping

The Second Research Academy of CASIC,Beijing 100854,China

Received:2017-07-18 Revised:2017-08-14 Online:2018-02-28 Published:2020-11-25

摘要/Abstract

摘要： 基于传统的固体动力及涡喷动力战术导弹质量估算模型,建立以冲压动力远程战术导弹的燃料质量及起飞质量的迭代质量估算模型,同时建立将末制导纳入质量估算的改进估算模型。使用改进前后的质量估算模型分别对按照固定目标及运动目标设计的飞行任务剖面进行仿真,将2种模型计算出的质量估算结果与基准导弹飞行弹道结果进行了对比验证,定量分析了改进前后估算误差来源;同时研究分析了射程、目标运动速度、末制导启动距离、巡航高度对改进前后估算模型误差的影响,提出对于较近射程的固定目标或低速目标可以使用传统的末制导简化质量估算模型,而对远射程、较高巡航高度、较大末制导启动距离以及具有高运动速度的目标应考虑将末制导加入质量估算模型或对改进前的质量估算模型进行二次修正以减少估算误差。

关键词: 冲压发动机, 战术导弹, 快速估算, 起飞质量, 迭代法, 数值仿真

Abstract: Based on the traditional mass evaluation model, an iterative evaluation model to study the fuel mass and the take-off mass of tactical scramjet missile is devised, and an improved evaluation model is put forward by taking terminal guidance into account. By comparing these two kinds of evaluation models for fixed and moving targets, the source of evaluation error is achieved. The influence of range, target speed, distance of terminal guidance and cruise height on evaluation error is discussed. The simulation results show that the traditional mass evaluation model which ignores the terminal guidance is suitable for short range fixed targets and low speed targets, while the mass-evaluation model considering terminal guidance or modified model ignoring the terminal guidance are suitable for long range, high cruise height, long-distance terminal guidance and high speed targets.

Key words: ramjet, tactical missile, evaluation, take-off mass, iteration method, numerical simulation

中图分类号:

王宏涛, 石德平. 冲压动力远程导弹燃料及起飞质量快速估算[J]. 现代防御技术, 2018, 46(1): 47-55.

WANG Hong-tao, SHI De-ping. Evaluation of Fuel and Take-off Mass for Tactical Scramjet Missile[J]. Modern Defense Technology, 2018, 46(1): 47-55.

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冲压动力远程导弹燃料及起飞质量快速估算

Evaluation of Fuel and Take-off Mass for Tactical Scramjet Missile

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