1[3]Bronowicki A J.Vibration isolator for large space telescope[J].AIAA Journal of Spacecraft & Rockets,2005.
2[5]Keith K,Denoyer,Conor Johnson.Recent Achievements in Vibra-tion Isolation Systems for Space Launch and On-Orbit Applications.52nd International Astronautical Congress Toulouse,France,October 1-5,2001.
3[6]Wilke P S,Alto P,Johnson C D,et al.Payload isolation system for launch vehicles[C]//SPIE Proceedings,1997,3045:20-30.
4[7]Conor D,Johnson,Paul S,Wilke.Protecting Satellites from the Dy-namics of the Launch Environment.2004 S/C & L/V DYNAMICS ENVIRONMENTS WORKSHOP June 23,2004.
6[12]Eugene R,Peter M,Wugner,Brandon J,et al.Multiple payload adaptors for low cost access to space[A].AIAA Space 2001-Coufer-ence and Exposition,Albuquerque,NM,Aug.28-30,2001.
7[13]Johnson C D,Wilke P S,Grosserode P J.Whole-spacecraft vibration isolation system for the GFO/Taurns mission[J].SPIE Proceedings,1999,3672:175-185.
8[14]Wilke P S,Johnson C D,Foenesa E R.Whole-spaenornft passive launch isolation[J].Journal of Spacecraft and Rockets,1998,35(5):690-694.
9[15]U.S.Patent Documents.Patent number:6012680.Jan.U,2000.Edberg et al.
10[16]Johnsou C D.On the design and testing of a spacecraft lounch vibra-tion isolation system (LVIS)[C]//Proneedings of the 38th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Mete-rials Conference,1997