Data Description

This page summarizes information about the selected resource and its origin based on SPASE metadata.

Table of Contents

  1. Product
  2. Repository
  3. Instruments
  4. Observatory
  5. Persons

SPASE version 2.0.0

Numerical Data Product: Pioneer 11 hourly merged magnetic field and plasma data

Resource ID
spase://VHO/NumericalData/Pioneer11/MAGandPLS/PT1H Get XML
Name
Pioneer 11 hourly merged magnetic field and plasma data
Description

This is an hourly resolution, merged magnetic field and plasma data set created at NSSDC for COHOWeb. Magnetic field vectors and plasma flow direction angles are given in RTN coordinates. Spacecraft position data are given in Heliographic inertial (HGI coordinates).

Additional information
nssdcftp readme
Acknowledgement

Please acknowledge the magnetic field and plasma Principal Investigators, Drs. E. Smith and P. Gazis, and NSSDC or GSFC-SPDF

Contact
Role Person
1. Principal investigator Dr. Edward J. Smith Get XML
2. Principal investigator Dr. Paul R. Gazis Get XML
3. General contact Dr. Natalia E. Papitashvili Get XML
Release date
2009-05-20 19:08:28
Repository
Name
SPDF Get XML
Availability
Online
Access rights
Open
URL
nssdcftp

for annual files via ftp

COHOWeb plots and lists

Pioneer 11-specific page for plots and lists

COHOweb top page

Plots, lists, scatter plots, regressions, distributions, means, etc.

Format
Text
File size
1 MB per 1 year
Acknowledgement

Please acknowledge the magnetic field and plasma Principal Investigators, Drs. E. Smith and P. Gazis, and NSSDC or GSFC-SPDF

Instruments
Magnetic Fields Get XML
Quadrispherical Plasma Analyzer Get XML
Measurement type
Magnetic field
Thermal plasma
Temporal description
Start date
1973-04-06 00:00:00
Stop date
1992-08-01 00:00:00
Note

Plasma data do not start until day 111 of 1973. Plasma data end on day 150 of 1992. Field and plasma data become increasingly sparse after the early 1980's.

Cadence
1 hour
Observed regions
Heliosphere.Outer

Parameters

Parameter #1

Name
Year
Parameter key
Column1
Description

Four digit Year

Cadence
1 hour
Fill value
999.9999
Parameter type
Temporal

Parameter #2

Name
Day
Parameter key
Column2
Description

Decimal Day of Year

Cadence
1 hour
Fill value
999.9999
Parameter type
Temporal

Parameter #3

Name
Hour
Parameter key
Column3
Description

Hour

Cadence
1 hour
Fill value
999.9999
Parameter type
Temporal

Parameter #4

Name
P10 radial distance
Parameter key
Column04
Description

Heliocentric radial distance of Pioneer 11 in AU

Cadence
1 hour
Units
AU
Parameter type
Positional

Parameter #5

Name
P10 latitude
Parameter key
Column05
Description

Heliographic Inertial elevation angle of Pioneer 11 in deg

Cadence
1 hour
Units
deg
Coordinate system
Spherical HGI
Parameter type
Positional

Parameter #6

Name
P10 longitude
Parameter key
Column06
Description

Heliographic Inertial azimuthal angle of Pioneer 11 in deg

Cadence
1 hour
Units
deg
Coordinate system
Spherical HGI
Parameter type
Positional

Parameter #7

Name
Magnetic Field Vector
Description

Hourly averages of RTN components of fine time scale magnetic field vectors

Cadence
1 hour
Units
nT
Coordinate system
Cartesian RTN
Structure
Size
3
Description

R,T,N components

Elements
Index Name Component Parameter key
1 R component I Column07
2 T component J Column08
3 N component K Column09
Fill value
999.9999
Quantity
Magnetic field
Qualifier
Vector

Parameter #8

Name
Magnetic Field Magnitude
Parameter key
Column10
Description

Hourly average of fine time scale magnetic field magnitudes

Cadence
1 hour
Units
nT
Fill value
999.9999
Quantity
Magnetic field
Qualifier
Magnitude

Parameter #9

Name
Flow speed
Parameter key
Column11
Description

Hourly averaged solar wind plasma flow speed

Cadence
1 hour
Units
km/s
Fill value
9999.9
Particle type
Proton
Quantity
Flow speed
Qualifier
Average

Parameter #10

Name
Flow elevation angle
Parameter key
Column12
Description

Hourly averaged solar wind plasma flow elevation angle

Cadence
1 hour
Units
deg
Coordinate system
Spherical RTN
Fill value
9999.9
Particle type
Proton
Quantity
Flow velocity
Qualifier
Elevation angle

Parameter #11

Name
Flow azimuth angle
Parameter key
Column13
Description

Hourly averaged solar wind plasma flow azimuthal angle

Cadence
1 hour
Units
Coordinate system
Spherical RTN
Fill value
9999.9
Particle type
Proton
Quantity
Flow velocity
Qualifier
Azimuth angle

Parameter #12

Name
Density
Parameter key
Column14
Description

Hourly averaged solar wind plasma density

Cadence
1 hour
Units
n/cc
Fill value
999.9999
Particle type
Proton
Quantity
Number density
Qualifier
Average

Parameter #13

Name
Temperature
Parameter key
Column15
Description

Hourly averaged solar wind plasma temperature

Cadence
1 hour
Units
degK
Fill value
9999999.
Particle type
Proton
Quantity
Temperature
Qualifier
Average

SPASE version 2.0.0

Instrument: Magnetic Fields

Instrument ID
spase://SMWG/Instrument/Pioneer11/MAG1 Get XML
Name
Magnetic Fields
Description

The magnetometer on Pioneer 11 was a triaxial helium magnetometer with seven dynamic ranges, from plus or minus 2.5 nT to plus or minus 1.0E-3 T. The linearity was 0.1% and the noise threshold was 0.01 nT rms for 0-1 Hz. The accuracy was 0.5% of full scale range. The experimenter used RTN coordinates in the data analysis. In this system, R (or X) is radially outward from the sun, T (or Y) was parallel to the sun's equatorial plane and had its direction given by the cross product of the sun's spin vector into the radial direction (i.e., into R), and N (or Z) completed the right-handed orthogonal system (positive northward). A detailed instrument description may be found in Smith et al., IEEE Trans. On Magnetics, v. M-11, p. 962, July 1975. Data include the interplanetary region.

Additional information
NSSDC's Master Catalog

Information about the Magnetic Fields experiment on the Pioneer 11 mission.

Contact
Role Person
1. Principal investigator Dr. Edward J. Smith Get XML
Release date
2009-05-20 21:10:01
Instrument type
Magnetometer
Investigation name
Magnetic Fields on Pioneer 11
Observatory
Pioneer 11 Get XML

SPASE version 2.0.0

Instrument: Quadrispherical Plasma Analyzer

Instrument ID
spase://SMWG/Instrument/Pioneer11/PLS Get XML
Name
Quadrispherical Plasma Analyzer
Description

The instrument consisted of dual 90-deg quadrispherical electrostatic analyzers, one with 26 individual particle detectors and the other with 5 current collectors. The system was capable of measuring incident plasma distribution parameters over the energy range 0.1 to 18 keV for protons and approximately 1 to 500 eV for electrons. The high-resolution analyzer with a constant of 9 keV/Q per kV applied to the plates, had a mean plate radius of 9 cm and separation of 0.5 cm. This analyzer was used to measure ions only, and had 26 channeltrons mounted on the semicircular exit to the analyzer. The aperture pointed through a wide slit in the back of the spacecraft high-gain antenna reflector and pointed along the spin axis toward the earth (and therefore the sun). The edges of the antenna reflector limited the viewing of the instrument to 73 deg with respect to the spin axis. The channeltrons covered a range of plus or minus 51 deg. Each channeltron near the center covered 3 deg and approximately 8 deg near the edges of the analyzer. The angular width perpendicular to the long angular width was about 2 deg. In half the spin period the whole cone of half-angle 51 deg centered on the sun was swept out. A medium-energy analyzer with a mean radius of 12 cm and a 1-cm plate separation (constant of 6 keV/Q per kV applied) was used to detect both ions and electrons. The detectors were five flat-surface current collectors. The three center collectors each covered 15 deg and covered the angular range of plus or minus 22.5 deg from the spin axis. The two outside collectors had an angular width of 47.5 deg and were located at plus or minus 46.25 deg from the center of the analyzer. There was a variety of possible operating modes for the experiment; however, the principal mode utilized during the encounter phase was one in which the analyzer plate potential was stepped through its range every one-half revolution of the spacecraft, and all current collectors or channeltrons were read out at the peak flux roll angle. The high and medium resolution analyzers operated independently, so a cross check between these analyzers was possible. The dynamic range for the particle fluxes was from 1.0E+2 to 3.0E+9/(sq cm-s) and the proton temperature down to 2.0E+3 deg K could be ascertained. Data include the interplanetary region. Detector A was turned off on September 16, 1987.

Additional information
NSSDC's Master Catalog

Information about the Quadrispherical Plasma Analyzer experiment on the Pioneer 11 mission.

Contact
Role Person
1. Principal investigator Dr. Aaron Barnes Get XML
Release date
2009-05-20 21:10:01
Instrument type
Quadrispherical Analyser
Investigation name
Quadrispherical Plasma Analyzer on Pioneer 11
Observatory
Pioneer 11 Get XML

SPASE version 2.0.0

Observatory: Pioneer 11

Observatory ID
spase://SMWG/Observatory/Pioneer11 Get XML
Name
Pioneer 11
Alternate name
1973-019A
Pioneer-G
Description

Pioneer 11 was the second mission to investigate Jupiter and the outer solar system and the first to explore the planet Saturn and its main rings. Pioneer 11, like Pioneer 10, used Jupiter's gravitational field to alter its trajectory radically. It passed close to Saturn and then it followed an escape trajectory from the solar system.

The spacecraft was 2.9 m long and contained a 2.74-m diameter high-gain antenna of aluminum honeycomb sandwich material whose feed was topped with a medium-gain antenna. A low-gain, omnidirectional antenna was mounted below the high-gain dish. The spacecraft contained two nuclear electric-power generators, which generated 144 W at Jupiter, but decreased to 100 W at Saturn. There were three reference sensors: a star (Canopus) sensor, and two sun sensors. Attitude position could be calculated from the reference direction to the earth and the sun, with the known direction to Canopus as backup. Pioneer 11's star sensor gain and threshold settings were modified, based on experience gained from the settings used on Pioneer 10. Three pairs of rocket thrusters provided spin-axis control (maintained at 4.8 rpm) and change of the spacecraft velocity. The thrusters could be either fired steadily or pulsed, by command.

Communications were maintained via the omnidirectional and medium-gain antennas, which operated together, connected to one receiver, while the high-gain antenna was connected to the other receiver. The receivers could be interchanged by command. Two radio transmitters, coupled to two traveling-wave tube amplifiers, produced 8 W power each in S-band. Communication uplink (earth to spacecraft) operated at 2110 MHz, and downlink (spacecraft to earth) at 2292 MHz. At Jupiter's distance, round-trip communication time took 92 min. Data were received at the Deep Space Network (DSN). The spacecraft was temperature-controlled to between -23 and +38 deg C (-10 to +100 deg F). An additional experiment, a low-sensitivity fluxgate magnetometer, was added to the Pioneer 11 payload.

Instruments studied the interplanetary and planetary magnetic fields; solar wind properties; cosmic rays; transition region of the heliosphere; neutral hydrogen abundance; distribution, size, mass, flux, and velocity of dust particles; Jovian aurorae; Jovian radio waves; the atmospheres of planets and satellites; and the surfaces of Jupiter, Saturn, and some of their satellites. Instruments carried for these experiments were magnetometer, plasma analyzer (for solar wind), charged-particle detector, ionizing detector, non-imaging telescopes with overlapping fields of view to detect sunlight reflected from passing meteoroids, sealed pressurized cells of argon and nitrogen gas for measuring penetration of meteoroids, UV photometer, IR radiometer, and an imaging photopolarimeter, which produced photographs and measured the polarization. Further scientific information was obtained from celestial mechanics and occultation phenomena.

This spacecraft, like Pioneer 10, contains a plaque that has a drawing depicting man, woman, and the location of the sun and earth in the galaxy.

During its closest approach, December 4, 1974, Pioneer 11 passed to within 34,000 km of Jupiter's cloud tops. It passed by Saturn on September 1, 1979, at a distance of 21,000 km from Saturn's cloud tops. The spacecraft has operated on a backup transmitter since launch. Instrument power sharing began in February 1985 due to declining RTG power output. Science operations and daily telemetry ceased on September 30, 1995 when the RTG power level was insufficient to operate any experiments. As of the end of 1995 the spacecraft was located at 44.7 AU from the Sun at a nearly asymptotic latitude of 17.4 degrees above the solar equatorial plane and was heading outward at 2.5 AU/year.

Additional information
NSSDC's Master Catalog

Information about the Pioneer 11 mission

Contact
Role Person
1. Project scientist Dr. Palmer Dyal Get XML
Release date
2009-05-20 20:00:12
Observatory group
PIONEER
Location
Region
Heliosphere.NearEarth

SPASE version 2.0.0

Person: Dr. Edward J. Smith

Name
Dr. Edward J. Smith
Organization
Jet Propulsion Laboratory
Email
edward.j.smith@jpl.nasa.gov
Phone
+1-818-354-2248
Person ID
spase://SMWG/Person/Edward.J.Smith Get XML
Release date
1999-08-18 00:00:00

SPASE version 2.0.0

Person: Dr. Paul R. Gazis

Name
Dr. Paul R. Gazis
Organization
NASA Ames Research Center
Person ID
spase://SMWG/Person/Paul.R.Gazis Get XML

SPASE version 2.0.0

Person: Dr. Natalia E. Papitashvili

Name
Dr. Natalia E. Papitashvili
Organization
GSFC-Code 612.4
Person ID
spase://SMWG/Person/Natalia.E.Papitashvili Get XML

SPASE version 2.0.0

Person: Ms. Tamara J. Kovalick

Name
Ms. Tamara J. Kovalick
Organization
GSFC-Code 672
Email
Tamara.J.Kovalick@nasa.gov
Phone
+1-301-286-9422
Person ID
spase://SMWG/Person/Tamara.J.Kovalick Get XML
Release date
2008-03-19 00:00:00

SPASE version 2.0.0

Person: Mr. Robert M. Candey

Name
Mr. Robert M. Candey
Organization
NASA Goddard Space Flight Center
Address
Code 672, Greenbelt, MD 20771, USA
Email
robert.m.candey@nasa.gov
Phone
1-301-286-6707
Person ID
spase://SMWG/Person/Robert.M.Candey Get XML
Release date
2007-05-30 19:43:56

SPASE version 2.0.0

Person: Dr. Robert E. McGuire

Name
Dr. Robert E. McGuire
Organization
NASA Goddard Space Flight Center
Address
Code 672, Greenbelt, MD 20771, USA
Email
mcguire@mail630.gsfc.nasa.gov
Phone
1-301-286-7794
Person ID
spase://SMWG/Person/Robert.E.McGuire Get XML
Release date
2007-05-30 15:25:24

SPASE version 2.0.0

Person: Dr. Aaron Barnes

Name
Dr. Aaron Barnes
Organization
NASA Ames Research Center
Person ID
spase://SMWG/Person/Aaron.Barnes Get XML

SPASE version 2.0.0

Person: Dr. Palmer Dyal

Name
Dr. Palmer Dyal
Organization
Retired - formerly at NASA-ARC
Person ID
spase://SMWG/Person/Palmer.Dyal Get XML
Release date
1999-08-18 00:00:00

SPASE version 1.3.0

Repository: SPDF

Repository ID
spase://SMWG/Repository/NASA/GSFC/SPDF Get XML
Name
SPDF
Description

Space Physics Data Facility

Additional information
SPDF

Space Physics Data Facility

Contact
Role Person
1. General contact Ms. Tamara J. Kovalick Get XML
2. Technical contact Mr. Robert M. Candey Get XML
3. Project scientist Dr. Robert E. McGuire Get XML
Release date
2008-08-26 21:02:30
Prior IDs
spase://vspo/repository/61
spase://SMWG/Repository/SPDF