Snecma propulsion solide advanced technology SRM nozzles, history and future

Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference

Volumn 4, Issue , 2006, Pages 2888-2903

  Berdoyes, Michel ^a,b,c  

^a SNECMA   (France)

^b Nozzle Design Department   (France)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLIGHT SYSTEMS; HOT GAS THRUST VECTOR CONTROL NOZZLES; PROPULSION SOLIDE; SUPERSONIC SPLITLINE;

CARBON; COMPOSITE MATERIALS; LIQUID PROPELLANTS; PROPULSION; ROCKET ENGINES; THERMODYNAMIC STABILITY;

NOZZLES;

EID: 34249284455     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (17)

1. Development of a 4-D reinforced C-C composite. AIAA paper 76-607, M .A. Maistre. Société Européenne de Propulsion. France.
2. Carbon-carbon materials for nozzles of Solid Propellant rocket motors. AIAA paper 76-609, J.J. Choury. Société Européenne de Propulsion. France.
3. Recent improvements in 4-D Carbon-carbon Materials. AIAA paper 77-822. P. Lamicq. Société Européenne de Propulsion. France
4. Novoltex® Textures For Thermostrucrural Materials. AIAA-91-1848. M. Montaudon, F. Fenot, F. Christin and JChoury, Société Européenne de Propulsion, Saint Médard en Jalles, France.
5. Improvements in Mechanical Analysis of Multi-Directional Sepcarb® Carbon-Carbon Composites. AIAA-84-1308. L. Delneste, Société Européenne de Propulsion, Saint Médard en Jalles, France.
6. Analysis of Solid Rocket Motor Nozzle AIAA-92-3616. P. Lapp and B. Quesada, Société Européenne de Propulsion, Saint Médard en Jalles, France.
7. Demonstration of the feasibility of an all-composite Space Motor. AIAA-83-1185. P. Donguy, Société Européenne de Propulsion, Saint Médard en Jalles, France; and R. A. Ellis and W. J. Kearney, Chemical System Div., United Technologies, Sunnyvale, Ca.
8. Hot Gas Thrust Vector Control Motor. AIAA-92-3551. M. Berdoyes, Société Européenne de Propulsion, Saint Médard en Jalles, France and Russell. A. Ellis, CSD PO box 49028 San José, CA 95161-9028.
9. Berdoyes Michel, Camy Pierre, Snecma Propulsion Solide - Le Haillan, France. Patent US 61170256 /EP 098446 - Anchor device for a member for actuating a steerable nozzle.
10. IAA-01-IAA.3.2.01- An Example of Successful International Cooperation in Rocket Motor Technology-Russell A. Ellis, Pratt & Whitney, San Jose, CA, U.S.A. and Michel Berdoyes, Snecma Moteurs, Le Haillan, France
11. Development and testing of Carbon-Carbon Valves and Tubings for Hot Gas Flow Control. AIAA 87-1820. J.F Sevellec, Société Européenne de Propulsion, Saint Médard en Jalles, France.
12. SEP Demonstrates Composite Valves for GBI. Defense Daily. March 6th 1990. p 353
13. Design and Development of a New SRM Nozzle Based on Carbon-Carbon and Carbon-Ceramic Materials. AIAA-88-3333 - P. Gentil, Société Européenne de Propulsion, Saint Médard en Jalles, France.
14. Improvement in Composite tactical Solid Rocket Motor Technology. AIAA -90-1975- D. Crapiz.-Société Européenne de Propulsion. Le Haillan, France.
15. Testing of Novoltex® 3-D Carbon-Carbon Integral Throat and Exit Cones (ITECs). AIAA 1998-3361. Russell A Ellis, United Technologies - Chemical Systems Division, San Jose- CA, USA
16. Vega program - The P80 FW SRM nozzle. AIAA 2004-4219- Gautronneau Snecma Propulsion Solide - Le Haillan (Bordeaux) - France, C. Cros ESA - P80 IPT - Evry (Paris) - France, Ph. Pascal CNES - P80 IPT - Evry (Paris) - France, M. Cutroni Europropulsion - Suresnes (Paris) - France
17. Sustainable C2 Rayon-Based Carbon Cloth for the Ariane 5 SRM Nozzle. AIAA 2005-3795 - Michel Berdoyes - Bernard Broquere, Sylvie Loison, Martine Dauchier, Snecma Propulsion Solide - Le Haillan, France.