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

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

著者名:

B. Favini ( Aeronautics, University of Rome - La Sapienza -, Rome, Italy )

M. Di Giacinto

A. Attili

D. Scoccimarro ( AVIO GROUP, Colleferro, Italy )

M. Biagioni

R. De Amicis

A. Neri ( ELV, Colleferro, Italy )

P. Bellomi

S. Bianchi ( VEGA IPT ESA/ESRIN, Rome, Italy )

F. Serraglia

M. Bonnet

さらに 6 件

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

シリーズ巻号:

2006

発行年:

2006

通号:

2006-5277

ペーパー番号:

AIAA Paper 2006-5277

出版情報:

Reston, Va: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200617 [CD-ROM 2006 Disc 17]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00047243
シリーズID:	PA00000151
会議名:	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
回次:	42nd
会議開催地:	Sacramento, California
会議開催年:	2006.07.09-2006.07.12

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1 テクニカルペーパー Internal Ballistics and Dynamics of VEGA Launcher Solid Rocket Motors During Ignition Transient: Firing Test Predictions and Post Firing Analysis M. Di Giacinto, B. Favini, A. Attili, F. Serraglia, D. Scoccimarro, C. Di Trapani American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Two Approaches for Condensed-Phase Modeling in Solid Rocket Motor Flows F. Creta, A. Attili, B. Favini, M. Di Giacinto American Institute of Aeronautics and Astronautics
2 国際会議録 GASDYNAMIC FEATURES IN SOLID ROCKET MOTORS WITH FINOCYL GRAIN DURING IGNITION TRANSiENT Serraglia, F., Favini, B., Di Giacinto, M., Neri, A. ESA Publications Division	8 国際会議録 A Simplified Coupled Structural-Flowfield Analysis of Solid Rocket Motors Ignition Transient E. Cavallini, B. Favini, F. Serraglia ESA Communications
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