High-impulse, low-power, digital microthrusters using low boiling temperature liquid propellant with high viscosity fluid plug
- 1 April 2002
- journal article
- Published by Elsevier in Sensors and Actuators A: Physical
- Vol. 97-98, 659-664
- https://doi.org/10.1016/s0924-4247(02)00030-4
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- An ink-jet head using diaphragm microactuatorPublished by Institute of Electrical and Electronics Engineers (IEEE) ,2002
- Digital MicroPropulsionPublished by Institute of Electrical and Electronics Engineers (IEEE) ,1999
- A Microinjector Free of Satellite Drops and Characterization of the Ejected DropletsPublished by ASME International ,1998
- Proof-of-concept demonstration of a vaporizing liquid micro-thrusterPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1998
- Design, analysis and fabrication of a vaporizing liquid micro-thrusterPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1997
- Thruster options for microspacecraft - A review and evaluation of existing hardware and emerging technologiesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1997
- Micromachined Acoustic-Wave Liquid EjectroPublished by Transducer Research Foundation Inc. (TRF) ,1996
- One-Dimensional Model of Bubble Growth and Liquid Flow in Bubble Jet PrintersJapanese Journal of Applied Physics, 1987