TY  - CONF
AU  - Scharlemann, C.
AU  - Schiebl, M.
AU  - Marhold, K.
AU  - Tajmar, M.
AU  - Miotti, P.
AU  - Guraya, C.
AU  - Seco, F.
AU  - Kappenstein, C.
AU  - Batonneau, Y.
AU  - Brahmi, R.
AU  - Lang, M.
PY  - 2006
DO  - 10.2514/6.2006-4551
SN  - 1563478188
SN  - 9781563478185
UR  - https://hdl.handle.net/11556/2352
AB  - The increasing application of microsatellites (from 10 kg up to 100 kg) for a rising number of various missions requires the development of suitable propulsion systems. Microsatellites have special requirements for a propulsion system such as small...
LA  - eng
PB  - American Institute of Aeronautics and Astronautics Inc.
TI  - Test of a turbo-pump fed miniature rocket engine
TY  - conference output
ER  -