Experimental measurement of particle deceleration and survival in multiple thin foil targets
Experimental results of deceleration of iron particles by means of a stack of thin Mylar foils are presented. The mass range of the iron particles is 3 x 10^-^1^2 to 1 x 10^-^1^08 the velocity ranges from 2.5 km/s to 5 km/s. Decelerations of up to ca. 70% were measured using 2 and 3 foils. The measu...
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| Autor*in: |
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| Format: |
E-Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
1986 |
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| Reproduktion: |
Elsevier Journal Backfiles on ScienceDirect 1907 - 2002 |
|---|---|
| Übergeordnetes Werk: |
in: Advances in Space Research - Amsterdam : Elsevier, 6(1986), 7, Seite 17-20 |
| Übergeordnetes Werk: |
volume:6 ; year:1986 ; number:7 ; pages:17-20 |
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| 245 | 1 | 0 | |a Experimental measurement of particle deceleration and survival in multiple thin foil targets |
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| 520 | |a Experimental results of deceleration of iron particles by means of a stack of thin Mylar foils are presented. The mass range of the iron particles is 3 x 10^-^1^2 to 1 x 10^-^1^08 the velocity ranges from 2.5 km/s to 5 km/s. Decelerations of up to ca. 70% were measured using 2 and 3 foils. The measured deceleration can be expressed over the whole velocity range studied as a function of the particle mass. Comparison with previous studies of thin foil penetration /1,2/ supports the approach to a scaling in terms of momentum conservation. We discuss limits for intact dust particle capture in space, and conclude that such techniques for deceleration and capture for comet flyby missions are effective. This is instanced already in Solar Max data where capture is effected at higher velocities and identifiable fragments of incident particles have been analysed. | ||
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(DE-627)NLEJ180350544 (DE-599)GBVNLZ180350544 DE-627 ger DE-627 rakwb eng Experimental measurement of particle deceleration and survival in multiple thin foil targets 1986 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier Experimental results of deceleration of iron particles by means of a stack of thin Mylar foils are presented. The mass range of the iron particles is 3 x 10^-^1^2 to 1 x 10^-^1^08 the velocity ranges from 2.5 km/s to 5 km/s. Decelerations of up to ca. 70% were measured using 2 and 3 foils. The measured deceleration can be expressed over the whole velocity range studied as a function of the particle mass. Comparison with previous studies of thin foil penetration /1,2/ supports the approach to a scaling in terms of momentum conservation. We discuss limits for intact dust particle capture in space, and conclude that such techniques for deceleration and capture for comet flyby missions are effective. This is instanced already in Solar Max data where capture is effected at higher velocities and identifiable fragments of incident particles have been analysed. Elsevier Journal Backfiles on ScienceDirect 1907 - 2002 Capaccioni, F. oth McDonnell, J.A.M. oth in Advances in Space Research Amsterdam : Elsevier 6(1986), 7, Seite 17-20 (DE-627)NLEJ180340476 (DE-600)2023311-5 0273-1177 nnns volume:6 year:1986 number:7 pages:17-20 http://linkinghub.elsevier.com/retrieve/pii/0273-1177(86)90205-X GBV_USEFLAG_H ZDB-1-SDJ GBV_NL_ARTICLE AR 6 1986 7 17-20 |
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(DE-627)NLEJ180350544 (DE-599)GBVNLZ180350544 DE-627 ger DE-627 rakwb eng Experimental measurement of particle deceleration and survival in multiple thin foil targets 1986 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier Experimental results of deceleration of iron particles by means of a stack of thin Mylar foils are presented. The mass range of the iron particles is 3 x 10^-^1^2 to 1 x 10^-^1^08 the velocity ranges from 2.5 km/s to 5 km/s. Decelerations of up to ca. 70% were measured using 2 and 3 foils. The measured deceleration can be expressed over the whole velocity range studied as a function of the particle mass. Comparison with previous studies of thin foil penetration /1,2/ supports the approach to a scaling in terms of momentum conservation. We discuss limits for intact dust particle capture in space, and conclude that such techniques for deceleration and capture for comet flyby missions are effective. This is instanced already in Solar Max data where capture is effected at higher velocities and identifiable fragments of incident particles have been analysed. Elsevier Journal Backfiles on ScienceDirect 1907 - 2002 Capaccioni, F. oth McDonnell, J.A.M. oth in Advances in Space Research Amsterdam : Elsevier 6(1986), 7, Seite 17-20 (DE-627)NLEJ180340476 (DE-600)2023311-5 0273-1177 nnns volume:6 year:1986 number:7 pages:17-20 http://linkinghub.elsevier.com/retrieve/pii/0273-1177(86)90205-X GBV_USEFLAG_H ZDB-1-SDJ GBV_NL_ARTICLE AR 6 1986 7 17-20 |
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(DE-627)NLEJ180350544 (DE-599)GBVNLZ180350544 DE-627 ger DE-627 rakwb eng Experimental measurement of particle deceleration and survival in multiple thin foil targets 1986 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier Experimental results of deceleration of iron particles by means of a stack of thin Mylar foils are presented. The mass range of the iron particles is 3 x 10^-^1^2 to 1 x 10^-^1^08 the velocity ranges from 2.5 km/s to 5 km/s. Decelerations of up to ca. 70% were measured using 2 and 3 foils. The measured deceleration can be expressed over the whole velocity range studied as a function of the particle mass. Comparison with previous studies of thin foil penetration /1,2/ supports the approach to a scaling in terms of momentum conservation. We discuss limits for intact dust particle capture in space, and conclude that such techniques for deceleration and capture for comet flyby missions are effective. This is instanced already in Solar Max data where capture is effected at higher velocities and identifiable fragments of incident particles have been analysed. Elsevier Journal Backfiles on ScienceDirect 1907 - 2002 Capaccioni, F. oth McDonnell, J.A.M. oth in Advances in Space Research Amsterdam : Elsevier 6(1986), 7, Seite 17-20 (DE-627)NLEJ180340476 (DE-600)2023311-5 0273-1177 nnns volume:6 year:1986 number:7 pages:17-20 http://linkinghub.elsevier.com/retrieve/pii/0273-1177(86)90205-X GBV_USEFLAG_H ZDB-1-SDJ GBV_NL_ARTICLE AR 6 1986 7 17-20 |
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(DE-627)NLEJ180350544 (DE-599)GBVNLZ180350544 DE-627 ger DE-627 rakwb eng Experimental measurement of particle deceleration and survival in multiple thin foil targets 1986 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier Experimental results of deceleration of iron particles by means of a stack of thin Mylar foils are presented. The mass range of the iron particles is 3 x 10^-^1^2 to 1 x 10^-^1^08 the velocity ranges from 2.5 km/s to 5 km/s. Decelerations of up to ca. 70% were measured using 2 and 3 foils. The measured deceleration can be expressed over the whole velocity range studied as a function of the particle mass. Comparison with previous studies of thin foil penetration /1,2/ supports the approach to a scaling in terms of momentum conservation. We discuss limits for intact dust particle capture in space, and conclude that such techniques for deceleration and capture for comet flyby missions are effective. This is instanced already in Solar Max data where capture is effected at higher velocities and identifiable fragments of incident particles have been analysed. Elsevier Journal Backfiles on ScienceDirect 1907 - 2002 Capaccioni, F. oth McDonnell, J.A.M. oth in Advances in Space Research Amsterdam : Elsevier 6(1986), 7, Seite 17-20 (DE-627)NLEJ180340476 (DE-600)2023311-5 0273-1177 nnns volume:6 year:1986 number:7 pages:17-20 http://linkinghub.elsevier.com/retrieve/pii/0273-1177(86)90205-X GBV_USEFLAG_H ZDB-1-SDJ GBV_NL_ARTICLE AR 6 1986 7 17-20 |
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(DE-627)NLEJ180350544 (DE-599)GBVNLZ180350544 DE-627 ger DE-627 rakwb eng Experimental measurement of particle deceleration and survival in multiple thin foil targets 1986 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier Experimental results of deceleration of iron particles by means of a stack of thin Mylar foils are presented. The mass range of the iron particles is 3 x 10^-^1^2 to 1 x 10^-^1^08 the velocity ranges from 2.5 km/s to 5 km/s. Decelerations of up to ca. 70% were measured using 2 and 3 foils. The measured deceleration can be expressed over the whole velocity range studied as a function of the particle mass. Comparison with previous studies of thin foil penetration /1,2/ supports the approach to a scaling in terms of momentum conservation. We discuss limits for intact dust particle capture in space, and conclude that such techniques for deceleration and capture for comet flyby missions are effective. This is instanced already in Solar Max data where capture is effected at higher velocities and identifiable fragments of incident particles have been analysed. Elsevier Journal Backfiles on ScienceDirect 1907 - 2002 Capaccioni, F. oth McDonnell, J.A.M. oth in Advances in Space Research Amsterdam : Elsevier 6(1986), 7, Seite 17-20 (DE-627)NLEJ180340476 (DE-600)2023311-5 0273-1177 nnns volume:6 year:1986 number:7 pages:17-20 http://linkinghub.elsevier.com/retrieve/pii/0273-1177(86)90205-X GBV_USEFLAG_H ZDB-1-SDJ GBV_NL_ARTICLE AR 6 1986 7 17-20 |
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Experimental results of deceleration of iron particles by means of a stack of thin Mylar foils are presented. The mass range of the iron particles is 3 x 10^-^1^2 to 1 x 10^-^1^08 the velocity ranges from 2.5 km/s to 5 km/s. Decelerations of up to ca. 70% were measured using 2 and 3 foils. The measured deceleration can be expressed over the whole velocity range studied as a function of the particle mass. Comparison with previous studies of thin foil penetration /1,2/ supports the approach to a scaling in terms of momentum conservation. We discuss limits for intact dust particle capture in space, and conclude that such techniques for deceleration and capture for comet flyby missions are effective. This is instanced already in Solar Max data where capture is effected at higher velocities and identifiable fragments of incident particles have been analysed. |
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Experimental results of deceleration of iron particles by means of a stack of thin Mylar foils are presented. The mass range of the iron particles is 3 x 10^-^1^2 to 1 x 10^-^1^08 the velocity ranges from 2.5 km/s to 5 km/s. Decelerations of up to ca. 70% were measured using 2 and 3 foils. The measured deceleration can be expressed over the whole velocity range studied as a function of the particle mass. Comparison with previous studies of thin foil penetration /1,2/ supports the approach to a scaling in terms of momentum conservation. We discuss limits for intact dust particle capture in space, and conclude that such techniques for deceleration and capture for comet flyby missions are effective. This is instanced already in Solar Max data where capture is effected at higher velocities and identifiable fragments of incident particles have been analysed. |
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Experimental results of deceleration of iron particles by means of a stack of thin Mylar foils are presented. The mass range of the iron particles is 3 x 10^-^1^2 to 1 x 10^-^1^08 the velocity ranges from 2.5 km/s to 5 km/s. Decelerations of up to ca. 70% were measured using 2 and 3 foils. The measured deceleration can be expressed over the whole velocity range studied as a function of the particle mass. Comparison with previous studies of thin foil penetration /1,2/ supports the approach to a scaling in terms of momentum conservation. We discuss limits for intact dust particle capture in space, and conclude that such techniques for deceleration and capture for comet flyby missions are effective. This is instanced already in Solar Max data where capture is effected at higher velocities and identifiable fragments of incident particles have been analysed. |
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