Design and development of a propulsion system for a cubesat - Based on solid propellant cool gas generator technology

AIAA 57th International Astronautical Congress, IAC 2006

Volumn 5, Issue , 2006, Pages 3434-3442

  Rackemann, N J ^a   Sanders, H M ^b   Van Vliet, L D ^b  

^a TECHNISCHE UNIVERSITÄT BERLIN   (Germany)

^b TNO   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

GAS GENERATORS; MATHEMATICAL MODELS; ORBITS; SOLID PROPELLANTS;

COOL GAS GENERATOR TECHNOLOGY; CUBESAT; ORBIT MANEUVERING;

SPACECRAFT PROPULSION;

EID: 41149090672     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. th Round Table on Micro/Nano Technologies for Space, 3-5 October 2005, ESTEC, Noordwijk, The Netherlands
2. th International Spacecraft Propulsion Conference (ESA SP-555). 2-9 June, 2004, Chia Laguna (Cagliari), Sardinia, Italy
3. Rackemann, N.J.; Design and Development of a Propulsion System for a Cubesat; TNO Defence, Security & Safety; 29 March 2006, Rijswijk, The Netherlands
4. Dekker, E.J; Feed System Minimization for Micro Propulsion, Final Report Aeronautical Engineering, TNO Defence, Security & Safety; 9 June 2006, Rijswijk, The Netherlands