1 |
Fosness, E.R., Buckley, S.J., & Gammill, W.F., "Deployment and Release Devices Efforts at the Air Force Research Laboratory Space Vehicles Directorate," AIAA Space 2001 Conference and Explosition, 2001, pp.28-30.
|
2 |
Muller J. and Anderau C., "High Load Low Shock Release Unit(30kN)," ESMATS 2009.
|
3 |
http://www.tiniaerospace.com.
|
4 |
Park, H.J., Tak, W.J. & Kim, B.K., "Shape Memory Alloy Actuator Based Non-explosive Low-shock Separation Device." KSAS Fall Conference, 2008, pp.1359-1364.
|
5 |
Kim K.W., Lee C.W., Jo Y.J., "Reliability Assessment of Tape Hinge Solar Array Deployment Mechanism", The Korea society for aeronautical & space sciences (KSAS) Fall Conference, 2006, pp.611-614.
|
6 |
Jang T.S., Kim H.B. Woo S.H., "Analysis on enviromental test specifcations for solar pnanels of STSAT-2," The Korea society for noise and vibration engineering(KSNVE) Fall Conference, 2005, pp.957-961.
|
7 |
ECSS-E-30 Part2A. ECSS Standards, 2000, pp.31
|
8 |
Hwang D.S., "Design and analysis of satellite structure," The Korea society for aeronautical & space sciences (KSAS) Fall Conference, 1994, pp.111-p121.
|
9 |
Lim J.H., Kim K.W., Kim S.W. Lee C.H., Rhee J.H., Hwang D.S., "Non-Explosive Actuator Technology for Satellite Applications," Korea Aerospace Research Institute(KARI), Vol.7, No.1, 2009, pp.97-104.
과학기술학회마을
|