TY  - CONF
AU  - Miotti, P.
AU  - Tajmar, M.
AU  - Guraya, C.
AU  - Perennes, F.
AU  - Marmiroli, B.
AU  - Soldati, A.
AU  - Campolo, M.
AU  - Kappenstein, C.
AU  - Brahmi, R.
AU  - Lang, M.
PY  - 2004
SN  - 1563477211
UR  - https://hdl.handle.net/11556/2461
AB  - Micro-satellites (from 10 kg up to 100 kg) have mass, volume, and electrical power constraints due to their low dimensions. These limitations lead to the lack in currently available active orbit control systems in micro-satellites. Therefore, a...
LA  - eng
TI  - Bi-propellant micro-rocket engine
TY  - conference output
ER  -