Remote sensing payload complex testing for youth australian-ukrainian microsatellite JAUESAT

1Bezuglyi, VA, 2Protsan, YV, 3Bondarenko, SG
1А. М. Makarov National Aerospace Educational Center of Youth, Dnipropetrovsk, Ukraine
2Oles Honchar National University of Dnipropetrovsk, Ukraine
3Oles Honchar National University of Dnipropetrovsk, Dnipropetrovsk, Ukraine
Kosm. nauka tehnol. 2003, 9 ;(Supplement1):024-028
Publication Language: Russian
The general of small/micro spacecrafts for space remote sensing researches requires of reliable operation for target board equipment in-orbit. A district of the launch of a satellite by space launch vehicle is characterized by definite combinations of various dynamic inputs/ loads adversely affecting the board satellite equipment. This combinations can not by fully modelled on the ground. In this case the efficiency can not by estimated in full measure. For more sharp estimation we propose to carry out the complex testing procedures with the use of the small non-controlled air rocket Zuni. By similar way the testing of Remote Sensing payload for JAUESAT will by conducted.
1. Aleksandrov V. A., Vladimirov V. V., Dmitriev R. D., Osipov S. O. Carrier rockets, 316 p. (Voenizdat, Moscow, 1981) [in Russian].

2. Volodin V. A., Tkachenko Yu. N. Construction and Design of Rocket Engines, Ed. by V. P. Sovetsky, 2nd revised and enlarged edition, 272 p. (Mashinostroenie, Moscow, 1984) [in Russian].