1968
DOI: 10.1109/tmag.1968.1066331
|View full text |Cite
|
Sign up to set email alerts
|

Space magnetics: The mariner V magnetometer experiment

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1
1

Citation Types

0
19
0

Year Published

1970
1970
2017
2017

Publication Types

Select...
4
1

Relationship

0
5

Authors

Journals

citations
Cited by 32 publications
(19 citation statements)
references
References 6 publications
0
19
0
Order By: Relevance
“…3: Verigin et al (1978). 4: Connor (1968). 5: http://nssdc.gsfc.nasa.gov/nmc/ experimentDisplay.do?id=1967-060A-04.…”
Section: A Brief Overview Of Space Physics Exploration At Venusmentioning
confidence: 99%
“…3: Verigin et al (1978). 4: Connor (1968). 5: http://nssdc.gsfc.nasa.gov/nmc/ experimentDisplay.do?id=1967-060A-04.…”
Section: A Brief Overview Of Space Physics Exploration At Venusmentioning
confidence: 99%
“…This point was emphasised by the modelling comparisons between Earth and Mars by Dryer and Heckman (1967) who concluded that the magnetic dipole moment of Mars was about 3 × 10 12 T m 3 , close to the possible value suggested by Smith et al (1965aSmith et al ( , 1965b. The magnetometer used on this mission was the first vector helium instrument (Connor 1968) that was to lead to a series of instruments on key planetary missions for the next 40 years. The schematic of the instrument is shown in Fig.…”
Section: Marsmentioning
confidence: 54%
“…However, It was not possible to exclude the possibility of a weak intrinsic magnetic field, but the close approach allowed to establish a much lowered upper limit, less than a fraction 1/400 of that of the Earth, than was possible with Mariner 2. The magnetometer on Mariner 5 was identical to the one flown on Mariner 4; it was the first time a quantum effect instrument, a Vector Helium Magnetometer was embarked on a planetary mission (Slocum and Reilly 1963;Connor 1968). This instrument is described in more detail in Sect.…”
Section: Venusmentioning
confidence: 99%
See 1 more Smart Citation
“…A comprehensive description of the instrument has been given by Connor (1968). There was an effort to reduce magnetic fields of the spacecraft by deperming it, and this 'led to a residual field of apprnoximately 8y, estimated both from terrestrial measurements and two axis estimates of the spacecraft field obtained during a short period of rolling of the spacecraft about the spacecraft-sun line shortly after launch.…”
Section: Lunar Experimentsmentioning
confidence: 99%