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.

Author(s):

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

6 more

Publication title:

AIAA meeting papers on disc

Title of ser.:

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

Ser. no.:

2006

Pub. Year:

2006

No.:

2006-5277

Paper no.:

AIAA Paper 2006-5277

Pub. info.:

Reston, Va: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200617 [CD-ROM 2006 Disc 17]

Type:

Technical Paper

Details

TDL ID:	ZA00047243
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Conf. info. (Number):	42nd
Conf. info. (Venue):	Sacramento, California
Conf. info. (Date):	2006.07.09-2006.07.12

Similar Items:

1 Technical Paper 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 Technical Paper 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 Conference Proceedings 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 Conference Proceedings A Simplified Coupled Structural-Flowfield Analysis of Solid Rocket Motors Ignition Transient E. Cavallini, B. Favini, F. Serraglia ESA Communications
3 Technical Paper Ignition Transient Pressure Oscillations in Solid Rocket Motors Favini, B., Di Giacinto, M., Serraglia, F. American Institute of Aeronautics and Astronautics	9 Technical Paper 3D Numerical Simulation of Ignition Transient in SRM B. Favini, S. Zaghi, F. Serraglia, M. Di Giacinto American Institute of Aeronautics and Astronautics
4 Conference Proceedings Numerical Simulation of Multiphase Flow in Solid Rocket Motors A. Attili, B. Favini, M. Di Giacinto, F. Serraglia ESA Communication Production Office	10 Technical Paper 3D Simulations of Pre-Ignition Transient of P80 SRM S. Zaghi, B. Favini, M. Di Giacinto, F. Serraglia American Institute of Aeronautics and Astronautics
5 Technical Paper A Fully Three Dimensional Analysis of Pre-Ignition Transient in Solid Rocket Motors B. Favini, S. Zaghi, F. Serraglia, M. Di Giacinto American Institute of Aeronautics and Astronautics	11 Technical Paper An Ignition-to-Burn Out Analysis of SRM Internal Ballistic and Performances M. Di Giacinto, B. Favini, E. Cavallini, F. Serraglia American Institute of Aeronautics and Astronautics
6 Technical Paper Modeling of Flowfield Features During Ignition Transients of Solid Rocket Motor. Favini, B., Giacinto, M.D., Serraglia, F. American Institute of Aeronautics and Astronautics	12 Technical Paper Vega Solid Rocket Motors: An Overview of 2006-2007 Development Activities S. Bianchi, M. Bonnet, F. Serraglia, F. Iasenzaniro, C. Milana American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12