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  - Eloirdi, R.
AU  - Lang, M.
PY  - 2004
UR  - https://hdl.handle.net/11556/4709
AB  - Micro-satellites (from 10kg up to 100kg) 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  -