Influence of spacecraft outgassing on the exploration of tenuous atmospheres with in situ mass spectrometry

被引:102
作者
Schlaeppi, B. [1 ]
Altwegg, K. [1 ]
Balsiger, H. [1 ]
Haessig, M. [1 ]
Jaeckel, A. [1 ]
Wurz, P. [1 ]
Fiethe, B. [2 ]
Rubin, M. [3 ]
Fuselier, S. A. [4 ]
Berthelier, J. J. [5 ]
De Keyser, J. [6 ]
Reme, H. [7 ,8 ]
Mall, U. [9 ]
机构
[1] Univ Bern, Inst Phys, CH-3012 Bern, Switzerland
[2] TU Braunschweig, Inst Comp & Network Engn, D-38106 Braunschweig, Germany
[3] Univ Michigan, AOSS, Ann Arbor, MI 48109 USA
[4] Lockheed Martin Adv Technol Ctr, Space Phys Dept, Dept ADCS, Palo Alto, CA 94304 USA
[5] LATMOS, F-94100 St Maur, France
[6] BIRA IASB, Space Phys Div, B-1180 Brussels, Belgium
[7] Univ Toulouse, UPS, CESR, F-31028 Toulouse 4, France
[8] CNRS, UMR 5187, Toulouse, France
[9] Max Planck Inst Sonnensyst Forsch, D-37191 Katlenburg Lindau, Germany
基金
瑞士国家科学基金会;
关键词
ROSETTA MISSION; RETURN FLUX; CONTAMINATION; INSTRUMENT; ORBIT; ION;
D O I
10.1029/2010JA015734
中图分类号
P1 [天文学];
学科分类号
0704 ;
摘要
In situ mass spectrometry has been a powerful tool in many space missions to investigate atmospheres and exospheres of different bodies in the solar system. Applying new technologies, the mass spectrometers have become increasingly more sensitive. In this study, we show that spacecraft outgassing, which can never be completely prevented, will be the limiting factor in future missions that investigate very tenuous atmospheres and exospheres of moons, asteroids, or comets at large heliocentric distances. The Rosetta Orbiter Spectrometer for Ion and Neutral Analysis (ROSINA) instrument on the European Space Agency Rosetta mission has monitored spacecraft outgassing for 6 years during #9the cruise phase with unprecedented instrument sensitivity. It is shown that diffusion of gas from materials and from the spacecraft interior plays an important role in maintaining a relatively permanent thin gas cloud around the spacecraft for many years. The density #9and composition of this gas cloud depends on location on the spacecraft, maneuvers, and payload activity. The main contaminants are water, which is adsorbed on cold surfaces, and organics from the spacecraft structure, electronics, and insulations. Decomposed lubricant material can give a significant contribution to the total background. Fortunately for Rosetta, outgassing of the spacecraft will play a minor role when the comet is close to perihelion; only in the early phase of the mission the outgassing may be larger than the cometary signature.
引用
收藏
页数:14
相关论文
共 33 条
[21]  
Pereira C, 2001, ESA SP PUBL, V480, P83
[22]   The flight spectral response of the ACIS instrument [J].
Plucinsky, PP ;
Schulz, NS ;
Marshall, HL ;
Grant, CE ;
Chartas, G ;
Sanwal, D ;
Teter, MA ;
Vikhlinin, AA ;
Edgar, RJ ;
Wise, MW ;
Allen, GE ;
Virani, SN ;
DePasquale, JM ;
Raley, MT .
X-RAY AND GAMMA-RAY TELESCOPES AND INSTRUMENTS FOR ASTRONOMY, PTS 1 AND 2, 2003, 4851 :89-100
[23]  
Robertson S. J., 1976, D496676 LMSCHREC TR
[24]   Asteroid exosphere:: A simulation for the ROSETTA flyby targets (2867) Steins and (21) Lutetia [J].
Schlaeppi, B. ;
Altwegg, K. ;
Wurz, P. .
ICARUS, 2008, 195 (02) :674-685
[25]   Rosetta target comet 67P/Churyumov-Gerasimenko -: Postperihelion gas and dust production rates [J].
Schulz, R ;
Stüwe, JA ;
Boehnhardt, H .
ASTRONOMY & ASTROPHYSICS, 2004, 422 (01) :L19-L21
[26]   COMPARISON OF SATELLITE SELF-CONTAMINATION EXPERIMENTS AND SCATTERING RETURN FLUX CALCULATIONS [J].
SCIALDONE, JJ ;
HEDIN, AE ;
RICE, CJ .
JOURNAL OF GEOPHYSICAL RESEARCH-SPACE PHYSICS, 1978, 83 (NA1) :195-198
[27]   A global kinetic model for cometary comae:: The evolution of the coma of the Rosetta target comet churyumov-gerasimenko throughout the mission [J].
Tenishev, Valeriy ;
Combi, Michael ;
Davidsson, Bjorn .
ASTROPHYSICAL JOURNAL, 2008, 685 (01) :659-677
[28]   Return flux of neutral and charged particles in geosynchronous orbit [J].
Thomas, PD ;
Fong, MC ;
Neier, KL .
OPTICAL SYSTEMS CONTAMINATION AND DEGRADATION, 1998, 3427 :290-301
[29]  
Tribble A.C., 2000, Fundamentals of Contamination Control, DOI DOI 10.1117/3.387881
[30]  
Uy O. M., 2003, ESA