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- SPACE ENVIRONMENT TESTBEDS Pre-NRA REQUIREMENTS WORKSHOP / March 29th - 30th

RADIATION MODEL USER FORUM... more


FLIGHT INVESTIGATIONS

Are a series of data gathering investigations, consisting either of a mission comprised of a complement of science investigations implemented as a piggyback payload, or as a standalone flight investigation in attached payload mode.

  • Collect data in space to validate the performance of new technology vulnerable to the effects of the solar varying environments and instruments for LWS science missions

  • Collect data in space to validate new and existing ground test protocols or mechanism models for the effects of solar variability on emerging technologies and components

FLIGHT INVESTIGATIONS NRA 02-OSS-04 SET-1; Awarded May 2003

FINAL AWARDS | PDF | 1 Page | 108KB

PAYLOAD EXPERIMENTS SELECTED FOR SET-1 MISSION
CREDANCE
Cosmic Radiation Environment Dosimetry and Charging Experiment
PI: Clive Dyer, QinetiQ/United Kingdom


DIME
Dosimetry Intercomparison and Miniaturization Experiment
PI: Peter McNulty, Clemson University


ELDRS
Development of Space-Based Test Platform for the Characterization of Proton Effects and Enhanced Low Dose Rate Sensitivity in Bipolar Junction Transistors
PI: Hugh Barnaby, Arizona State


COTS-2
Validation of Single Event Effects Mitigation via Fault Tolerant Methodology
PI: Robert Ecoffet, CNES/France


PolyRAD (alternate experiment)
Radiation Shielding Performance of PolyRAD
PI: Edward Long, Longhill Engineering


DATA INVESTIGATIONS

Data Investigations are the exploitation of data from independent space missions conducted in the past and present to improve, develop, and validate engineering environment models, tools, and databases for reliable spacecraft design and operations.


DATA INVESTIGATIONS NRA 8-31; Awarded March 2002

FINAL AWARDS Descriptions
PDF | 9 Pages | 1.7MB

FINAL REPORTS:
Modeling Charge Collection in Detector Arrays - J.C. Pickel
PDF | 40pgs | 9.6MB

Analysis of CRRES PHA Data for Low-Energy-Deposition Events - P.J. McNulty
PDF | 41pgs | 11.6MB

Mining CRRES IDM Pulse Data and CRRES Environmental Data to Improve Spacecraft Charging/Discharging Models and Guidelines - A.R. Frederickson
PDF | 55pgs | 1.1MB

Electrostatic Return on Contaminants - R. Rantanen

PDF | 62pgs | 18.9MB

Displacement Damage Effects in Solar Cells - Mining Damage From the Microelectronics and Photonics Test Bed Experiment - R.J. Walters
PDF | 43pgs | 2.9MB

TID Effects of High-Z Material Spot Shields on FPGA Using MPTB Data - S.H. Crain
PDF | 22pgs | 1.4MB

Solar Variability and the Near-Earth Environment-Mining Enhanced Low Dose Rate Sensitivity Data From the Microelectronics and Photonics Test Bed Space Experiment -
T. Turflinger

PDF | 133pgs | 6MB

Characterization of Magnetospheric Spacecraft Charging Environments Using the LANL Magnetospheric Plasma Analyzer Data Set - V.A. Davis
PDF | 111pgs | 3.3MB

FINAL PRODUCTS - Models & Databases Available to Community


PAYLOAD EXPERIMENTS FOR SET-1 MISSION

 

Cosmic Radiation Environment Dosimetry and Charging Experiment (CREDANCE)

PI: Dr. Clive Dyer, QinetiQ/United Kingdom

Objectives:
Characterize the energetic space radiation environment and its interactions with spacecraft
Provide data to other SET-1 experiments

Goals:
Provide data to improve radiation environment models and design tools
Demonstrate the value of a compact space weather monitor in operational spacecraft

Measurements:
Proton flux > 40 MeV per unit solid angle
Charge deposition in large silicon diodes arranged in telescopes. Pulse height analysis is used to obtain ion linear energy transfer (LET) spectra of heavy ions in the 100 MeV-cm2/g to 25000 MeV-cm2/g range
Threshold voltage shift as a function of time to measure total ionizing dose in silicon at 2 different shielding depths
Charging current at 3 different shielding depths to provide energetic electron flux measurements at 3 energies


Dosimetry Intercomparison and Miniaturization Experiment (DIME)

PI: Dr. Peter McNulty, Clemson University
Objectives:

Use five different COTS microdosimeters to characterize radiation induced total ionizing dose, displacement damage, and single event effects

Goals:

Provide data to permit appropriate dosimetry selection in future missions to characterize/resolve operational anomalies
Validate particle transport codes by varying shielding thicknesses on RADFETs

DIME Measurements:

RADFET – Radiation-Sensing Field-Effect Transistor
Threshold voltage shift as a function of time to measure total ionizing dose
EPROM - Erasable Programmable Read-only Memory
Threshold voltage shift as a function of time to measure total ionizing dose
Number of single event upsets as a function of time to measure rates as a function of radiation level
UVPROM – Ultraviolet erasable Programmable Read-only Memory
Charge stored on floating gates is neutralized with radiation exposure. Resulting bit flips reflect micro-dose deposited in gates
2 LET Spectrometers – Linear Energy Transfer Spectrometers
Pulse height spectra as function of time is converted to LET to measure ions including protons. Optimized for high and low LET ions.
OSL Films - Optically Stimulated Luminescent Films
Visible emission spectrum as a function of time gives sensitive measure of ionizing dose


Development of Space-Based Test Platform for the Characterization of Proton Effects and Enhanced Low Dose Rate Sensitivity (ELDRS) in Bipolar Junction Transistors

PI: Dr. Hugh Barnaby, Arizona State University
Objective:
Measure ELDRS (primary) and proton effects (secondary) in positive-negative-positive (PNP) bipolar junction transistors (BJTs)

Goal:

Improve understanding of the physics of ELDRS and thereby improve/validate ground testing protocol for linear bipolar technologies and reduce design margins

Measurement:

Base and collector currents for 24 COTS BJTs as functions of the emitter and gate voltages and time


COTS-2: Digital Technologies

PI: Robert Ecoffet, CNES/France
Objective:
Validate approaches to mitigate single event effects by comparing simulation techniques, performance models, and on-orbit data
Validate mitigation of single event effects during space weather events

Goal:

Increase reliability of COTS technologies for space applications and reduce design margins

Measurement:

Measure single event effects on COTS FPGAs, classify the event by event type, and determine if mitigation of the effect occurred without watchdog intervention


Radiation Shielding Performance of PolyRAD (alternate experiment)

PI: Edward Long, Longhill Engineering
Objective:

Evaluate the space flight performance of spot shielding with polyRAD for reduction of total ionizing dose

Goals:

Reduction of mass margins, cost and radiation damage risk
Enable space flight use of advanced COTS microelectronics

Measurement:

Threshold voltage shift of RADFETs to measure total ionizing dose for 2 shielding configurations:
2-dimensional flat shape corresponding to top-side shielding
3-dimensional net shape representing device encapsulation


 


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Last Updated: February 15, 2007