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. Instrument
  4. Observatory
  5. Persons

SPASE version 2.0.0

Numerical Data Product: P11 CRT 6-hr fluxes and rates

Resource ID
spase://VEPO/NumericalData/Pioneer11/CRT/PT6H Get XML
Name
P11 CRT 6-hr fluxes and rates
Description

This data set has eight 6-hour fluxes (3.45-5.15, 30.55-56.47 and 120.7-227.3 MeV protons, 3.44-4.97, 10.03-21.7, 30.67-56.7 and 112.7-413 MeV/n alpha particles, and 2-6 MeV electrons), 28 count rates, and Poisson uncertainties in the fluxes and rates, as determined from the Cosmic Ray Telescope (CRT) on the Pioneer 11 spacecraft. Data are in annual files with consistent end-of-record marks. Spacecraft position data are not given in the data records but are accessible from Helioweb at http://cohoweb.gsfc.nasa.gov/helios/heli.html

Additional information
Voldesc.sfdu
Format.sfdu
Acknowledgement

the Principal Investigator, Frank B. McDonald

Contact
Role Person
1. Principal investigator Dr. Frank B. McDonald Get XML
2. General contact Dr. Nand Lal Get XML
Release date
2008-11-10 20:20:54
Repository
Name
SPDF Get XML
Availability
Online
Access rights
Open
URL
FTPBrowser

For display and retrieval of parameter subsets

nssdcftp

For ftp downloading of annual files

Format
Text
File size
1.5 MB per 1 year
Acknowledgement

the Principal Investigator, Frank B. McDonald, and FTPBrowser at SPDF

Processing level
Calibrated
Instrument
Cosmic-Ray Telescope Get XML
Measurement type
Energetic particles
Temporal description
Start date
1973-04-02 00:00:00
Stop date
1994-12-31 00:00:00
Cadence
6 hours
Observed regions
Heliosphere.Outer

Parameters

Parameter #1

Name
Proton Flux 3.45-5.15 MeV
Description

This flux is obtained from LET-I and is derived from pulse height data using R11A for normalization

Units
particles/(cm**2 sec ster MeV)
Structure
Size
1
Fill value
0.000000e+00
Particle type
Proton
Quantity
Number flux
Qualifier
Average
Energy range
Low energy
3.45
High energy
5.15
Units
MeV

Parameter #2

Name
Proton Flux 30.55-56.47 MeV
Description

This flux is obtained from HET and is derived from pulse height data using R1 for normalization

Units
particles/(cm**2 sec ster MeV)
Structure
Size
1
Fill value
0.000000e+00
Particle type
Proton
Quantity
Number flux
Qualifier
Average
Energy range
Low energy
30.55
High energy
56.47
Units
MeV

Parameter #3

Name
Proton Flux 120.7-227.3 MeV
Description

This flux is obtained from HET and is derived from pulse height data using R2 for normalization

Units
particles/(cm**2 sec ster MeV)
Structure
Size
1
Fill value
0.000000e+00
Particle type
Proton
Quantity
Number flux
Qualifier
Average
Energy range
Low energy
120.7
High energy
227.3
Units
MeV

Parameter #4

Name
Helium Flux 3.44-4.97 MeV/n
Description

This flux is obtained from LET-1 and is derived from pulse height data using R11B for normalization

Units
particles/(cm**2 sec ster MeV/n)
Structure
Size
1
Fill value
0.000000e+00
Particle type
AlphaParticle
Quantity
Number flux
Qualifier
Average
Energy range
Low energy
3.44
High energy
4.97
Units
MeV/n

Parameter #5

Name
Helium Flux 10.03-21.7 MeV/n
Description

This flux is obtained from LET-1 and is derived from pulse height data using R11B for normalization

Units
particles/(cm**2 sec ster MeV/n)
Structure
Size
1
Fill value
0.000000e+00
Particle type
AlphaParticle
Quantity
Number flux
Qualifier
Average
Energy range
Low energy
10.03
High energy
21.7
Units
MeV/n

Parameter #6

Name
Helium Flux 30.67-56.7 MeV/n
Description

This flux is obtained from HET and is derived from pulse height data using R2B for normalization

Units
particles/(cm**2 sec ster MeV/n)
Structure
Size
1
Fill value
0.000000e+00
Particle type
AlphaParticle
Quantity
Number flux
Qualifier
Average
Energy range
Low energy
30.67
High energy
56.7
Units
MeV/n

Parameter #7

Name
Helium Flux 112.7-413 MeV/n
Description

This flux is obtained from HET and is derived from pulse height data using R3A for normalization

Units
particles/(cm**2 sec ster MeV/n)
Structure
Size
1
Fill value
0.000000e+00
Particle type
AlphaParticle
Quantity
Number flux
Qualifier
Average
Energy range
Low energy
112.7
High energy
413
Units
MeV/n

Parameter #8

Name
Electron Flux 2-6 MeV
Description

This flux is obtained from HET and is derived from pulse height data using R1 for normalization

Units
particles/(cm**2 sec ster MeV/n)
Structure
Size
1
Fill value
0.000000e+00
Particle type
Electron
Quantity
Number flux
Qualifier
Average
Energy range
Low energy
2
High energy
6
Units
MeV/n

Parameter #9

Name
Poisson uncertainties in fluxes
Description

These are the Poisson uncertainties in the eight fluxes named above as scalars. In the data records, each immediately follows the flux it refers to.

Units
particles/(cm**2 sec ster MeV/n)
Structure
Size
8
Fill value
-1.000000e+00
Particle type
Proton
AlphaParticle
Electron
Quantity
Number flux
Qualifier
Uncertainty

Parameter #10

Name
Count rates
Description

These are 28 6-hour-averaged count rates corresponding to various telescope sensors singly and in coincidence, and, for some, for various levels of energy deposition in sensors. The documentation cited above gives conditions for each rate: which sensors, which species (one or more), etc.

Units
particles/sec
Structure
Size
28
Fill value
0.000000e+00
Particle type
Proton
AlphaParticle
Electron
Quantity
Counts
Qualifier
Average

Parameter #11

Name
Count rate uncertainties
Description

These are Poisson uncertainties in each of the above-identified 28 6-hour-averaged count rates corresponding to various telescope sensors singly and in coincidence, and, for some, for various levels of energy deposition in sensors. The documentation cited above gives conditions for each rate: which sensors, which species (one or more), etc. The uncertainty for each count rate immediately follows that count rate in the data records.

Units
particles/sec
Structure
Size
28
Fill value
-1.000000e+00
Particle type
Proton
AlphaParticle
Electron
Quantity
Counts
Qualifier
Uncertainty

SPASE version 2.0.0

Instrument: Cosmic-Ray Telescope

Instrument ID
spase://SMWG/Instrument/Pioneer11/CRT Get XML
Name
Cosmic-Ray Telescope
Description

This experiment consisted of three 3-element telescopes, all looking normal to the spacecraft spin axis. A bidirectional telescope measured 20- to 800-MeV/nucleon particles with 5 to 10% energy resolution. Another telescope measured 3- to 22-MeV/nucleon particles with 5% resolution. These two telescopes measured particles with Z values between 1 and 8. The third telescope measured 50-keV to 1-MeV electrons and 50-keV to 20-MeV protons with 20% resolution. Data include the interplanetary region.

Additional information
NSSDC's Master Catalog

Information about the Cosmic-Ray Telescope experiment on the Pioneer 11 mission.

Contact
Role Person
1. Principal investigator Dr. Frank B. McDonald Get XML
Release date
2009-05-20 21:10:01
Instrument type
Energetic Particle Instrument
Investigation name
Cosmic-Ray Telescope 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. Frank B. McDonald

Name
Dr. Frank B. McDonald
Organization
University of Maryland
Email
fm27@umail.umd.edu
Phone
+1-301-405-4861
Person ID
spase://SMWG/Person/Frank.B.McDonald Get XML
Release date
2000-07-18 00:00:00

SPASE version 2.0.0

Person: Dr. Nand Lal

Name
Dr. Nand Lal
Organization
GSFC-Code 612.4
Person ID
spase://SMWG/Person/Nand.Lal 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. 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