论文信息 - ADN-BASED PROPULSION FOR SPACECRAFT -KEY REQUIREMENTS AND EXPERIMENTAL VERIFICATION

ADN-BASED PROPULSION FOR SPACECRAFT -KEY REQUIREMENTS AND EXPERIMENTAL VERIFICATION

This paper describes the ongoing work to develop a storable liquid monopropellant for spacecraft propulsion based on Ammoniumdinitramide, ADN, and related rocket engine technologies. The primary objective of this effort is to reduce operational hazards and improve performance as compared with monopropellant hydrazine. Previous papers 1,2,3,4 have described the basic properties of ADN, possible propellant compositions and experimental results from test firings of small rocket engines.

Kjell Anflo | Tor-Arne Grönland | Göran Bergman | Rikard Nedar

[1] Stacy Christofferson,et al. Performance and life testing of small HAN thrusters , 1999 .

[2] P. Korting,et al. High-performance propellants based on hydrazinium nitroformate , 1995 .

[3] Stacy Christofferson,et al. Assessment of high performance HAN-monopropellants , 2000 .

[4] Kjell Anflo,et al. Development and Testing of ADN-Based Monopropellants in Small Rocket Engines , 2000 .

[5] N. Wingborg,et al. The properties of ammonium dinitramide (ADN): Part 1, basic properties and spectroscopic data , 2000 .

[6] William A. Facinelli,et al. EXPERIMENTAL DEVELOPMENT OF A MONOPROPELLANT FOR SPACE PROPULSION SYSTEMS , 1997 .

[7] Dieter M. Zube,et al. Evaluation of HAN-Based Propellant Blends , 2003 .

[8] J.L.P.A. Moerel,et al. Industrial benefits of applying HNF in monopropellant satellite propulsion , 2001 .

[9] Kjell Anflo,et al. Towards Green Propulsion for Spacecraft with ADN-Based Monopropellants , 2002 .

[10] Robert S. Jankovsky,et al. HAN-based monopropellant assessment for spacecraft , 1996 .

[11] V. Bombelli,et al. Economic benefits of the use of non-toxic mono-propellants for spacecraft applications , 2003 .

[12] Gerry Brewster,et al. Development and testing of new, HAN-based monopropellants in small rocket thrusters , 1998 .