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Internal charging is generated by penetrative electrons from the outer radiation belt, and the resultant discharges usually occur inside spacecrafts or sdeeply in the surface dielectrics. Therefore it may produce more serious results in electronics on board compared with surface charging. In this article, the general characteristics of internal charging were introduced, and, as an example, an internal charging induced anomaly, which took place on Double Star (TC-1 and TC-2) was analyzed through correlation of the anomaly with high energetic electron enhancement. The analysis provides a typical instance for spacecraft anomaly diagnostics.
[1] ［1］Frederickson A R, Holeman E G, Mullen E G 1992 IEEE Trans. Nuc. Sci. 39 1773
[2] ［2］Frederickson A R, Mullen E G, Kerns K J, Robinson P A 1993 IEEE Trans. Nuc. Sci. 40 233
[3] ［3］Frederickson A R, Brautigam D H 2004 Mining CRRES IDM Pluse Data and CRRES Environment Data to lmprove Spacecraft Charging/Discharging Models and Guidelines,NASA/CR 2004-213228
[4] ［4］Han J W, Huang J G 2005 J. Spacecraft Rockets 42 1061
[5] ［5］Baker D N, Goldberg R A, Herraro F A, Blake J B, Callis L B 1993 J. Atmos. Terrest. Phys. 55 1619
[6] ［6］Vampola A L, Environment Modeliy for Space-based Appliation 1996 ESA SP-392 151
[7] ［7］Koons H C, Gorney D J, Blake J B 1994 J. Spacecraft Rockets 31 557
[8] ［8］Huang J G, Chen D 2004 Acta Phys. Sin. 53 961 (in Chinese) ［黄建国、陈东 2004 53 961 ］
[9] ［9］Huang J G, Chen D 2004 Acta Phys. Sin. 53 1611 (in Chinese) ［黄建国、陈东 2004 53 1611］
[10] ］Shu T L, Edmond M, William J M 2002 J. Spacecraft Rockets 39 106
[11] ］Levy L, Mandeville J C, Siguier J M, Reulet R, Sarrail D, Catani J P, Gerlach L 1997 IEEE Trans. Nuc. Sci. 44 2201
[12] ］Wrenn G L, Smith R J K 1996 IEEE Trans. Nuc. Sci. 43 2783
[13] ］Mulville D R 1999 Avoiding Problems Caused by Spacecraft On-Orbit lnternal Charging Effects NASA-HDBK-4002 1
[14] ］Violet M D, Frederickson A R 1993 IEEE Trans. Nuc. Sci. 40 1512
[15] ］Mullen E G, Gussehoven M S, Hardy D A, Aggson T A, Ledly B G, Whipple E 1986 J. Geophys. Res. 91 1464
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[1] ［1］Frederickson A R, Holeman E G, Mullen E G 1992 IEEE Trans. Nuc. Sci. 39 1773
[2] ［2］Frederickson A R, Mullen E G, Kerns K J, Robinson P A 1993 IEEE Trans. Nuc. Sci. 40 233
[3] ［3］Frederickson A R, Brautigam D H 2004 Mining CRRES IDM Pluse Data and CRRES Environment Data to lmprove Spacecraft Charging/Discharging Models and Guidelines,NASA/CR 2004-213228
[4] ［4］Han J W, Huang J G 2005 J. Spacecraft Rockets 42 1061
[5] ［5］Baker D N, Goldberg R A, Herraro F A, Blake J B, Callis L B 1993 J. Atmos. Terrest. Phys. 55 1619
[6] ［6］Vampola A L, Environment Modeliy for Space-based Appliation 1996 ESA SP-392 151
[7] ［7］Koons H C, Gorney D J, Blake J B 1994 J. Spacecraft Rockets 31 557
[8] ［8］Huang J G, Chen D 2004 Acta Phys. Sin. 53 961 (in Chinese) ［黄建国、陈东 2004 53 961 ］
[9] ［9］Huang J G, Chen D 2004 Acta Phys. Sin. 53 1611 (in Chinese) ［黄建国、陈东 2004 53 1611］
[10] ］Shu T L, Edmond M, William J M 2002 J. Spacecraft Rockets 39 106
[11] ］Levy L, Mandeville J C, Siguier J M, Reulet R, Sarrail D, Catani J P, Gerlach L 1997 IEEE Trans. Nuc. Sci. 44 2201
[12] ］Wrenn G L, Smith R J K 1996 IEEE Trans. Nuc. Sci. 43 2783
[13] ］Mulville D R 1999 Avoiding Problems Caused by Spacecraft On-Orbit lnternal Charging Effects NASA-HDBK-4002 1
[14] ］Violet M D, Frederickson A R 1993 IEEE Trans. Nuc. Sci. 40 1512
[15] ］Mullen E G, Gussehoven M S, Hardy D A, Aggson T A, Ledly B G, Whipple E 1986 J. Geophys. Res. 91 1464
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