Ignition Transient Induced Loads Control Strategy for VEGA Launcher' Solid Rocket Motors: the "Zefiro9" Static Firing Test Predictions and Post Firing Analysis. Zefiro9 Static Firing Test Predictions and Post-firing Analysis

Author:

Favini B,Di Giacinto M,Attili A,Scoccimarro D,Biagioni M,De Amicis R.,Neri A,Bellomi P.,Bianchi S,Serraglia F,Bonnet M

Publisher

American Institute of Aeronautics and Astronautics

Reference11 articles.

Cited by 7 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Parametric Study on Solid Rocket Motor Ignition Transient and Pressure Oscillations Onset;Journal of Propulsion and Power;2015-07

2. SRM Internal Ballistic Numerical Simulation by SPINBALL Model;45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2009-08-02

3. Post-Firing Analysis of Z23 SRM Ignition Transient;45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2009-08-02

4. Comparison Between Different Pressurant Gases for Ignition Transient of P80 SRM;45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2009-08-02

5. An Ignition-to-Burn Out Analysis of SRM Internal Ballistic and Performances;44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2008-07-21

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