Next generation launch and propulsion systems face significant challenges of providing increased performance at lower cost with shorter development cycles. The use of existing materials in new application areas and the development and application of "advanced" material systems are enabling for the achievement of these aggressive goals. An area which offers substantial opportunity to decrease liquid rocket engine systems weight, and thus provide a measure of increased performance, is the nozzle. This presentation will examine the technical issues and showstoppers limiting the application of alternate materials to liquid rocket engine nozzles and identify the key material systems which have the potential for high payoff relative to the forcing functions of cost and performance (weight). Existing nozzle material development projects will be cited and opportunities for future joint partnerships to address these materials and processes challenges will be addressed. The presentation will include overviews of activities in low cost ablative nozzles, ceramic matrix composite cooled and uncooled nozzles, and advanced metallics.
Technical Challenges for Next Generation Liquid Rocket Engine Nozzles
National Space and Missile Materials Symposium ; 1998 ; Colorado Springs, CO, United States
01.01.1998
Sonstige
Keine Angabe
Englisch
Advanced Rocket Engine Nozzles
British Library Conference Proceedings | 1996
|Advanced rocket engine nozzles
AIAA | 1996
|Aerothermodynamcis Issues for Future Liquid Rocket-Engine Nozzles
British Library Conference Proceedings | 2002
|Robotic Processing Of Rocket-Engine Nozzles
NTRS | 1994
|