QADHD point-kernel radiation shielding computer code to evaluate propellant heating and dose to crew during engine operation
Point-kernel radiation shielding computer program to evaluate propellant heating and dose to crew during engine operation
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Point-kernel radiation shielding computer program to evaluate propellant heating and dose to crew during engine operation
Field doses and angular distribution of gamma radiation from surface of isotropic sources at boundary separating two media
Primary and secondary particle radiation doses shielded from solar flare and Van Allen belt protons by aluminum and polyethylene slabs
Room temperature density-dose behavior of neutron and gamma irradiated polytetrafluoroethylene /PTFE/ noting crystallinity variations
Low dose reactor irradiation effect on temperature dependence of dynamic modulus and internal friction of as-deposited pyrolytic graphite
Synchronised populations of mouse C3H/10T-1/2 cells were obtained by a stringent mitotic dislodgment procedure. Mitotic cells rapidly attach and progress sequentially through the cell cycle. Irradiation (3 Gy of X rays) was carried out at intervals from 0 to 18 h after initiating cell cycle progression of the mitotic cells. Oncogenic transformation was enhanced 10-fold over cells irradiated soon after replating (G1 and S phases) for cells in a near 2 h period corresponding to cells in G2 phase but not in mitosis. The cell surviving fraction had a 2-1/2-fold variation with resistant peaks corresponding to the late G1 and late S phases. These findings provide experimental support for the hypothesis initiated by Rossi and Kellerer and developed by Brenner and Hall to explain the LET dependent inverse dose rate effect for oncogenic transformation.
This paper compares total dose effects on two different technology (CMOS and BiCMOS) 12-bit ADCs from the same manufacturer, Burr-Brown.
64Mb 3.3V CMOS DRAMs from two different manufacturers were tested for total dose. Retention time, power supply current, and functionality were used to characterize device response.
This paper discusses total dose effects on voltage-to-frequency converters which impose different requirements on internal circuitry, and are also very high-precision devices (for example, linearity is typically specified between 0.002 and 0.05%).
This paper compares low-paper op-amps, OPA241 (bipolar) and OPA336 (CMOS), from Burr-Brown, MAX473 (bipolar) and MAX409 (CMOS), characterizing their total dose response with a single 2.7V power supply voltage.
Total dose damage in bipolar integrated circuits is investigated at low temperature, along with the temperature dependence of the electrical parameters of internal transistors. Bandgap narrowing causes the gain of npn transistors to decrease far more at low temperature compared to pnp transistors, due to the large difference in emitter doping concentration. When irradiations are done at temperatures of -140 deg C, no damage occurs until devices are warmed to temperatures above -50 deg C. After warm-up, subsequent cooling shows that damage is then present at low temperature. This can be explained by the very strong temperature dependence of dispersive transport in the continuous-time-random-walk model for hole transport. For linear integrated circuits, low temperature operation is affected by the strong temperature dependence of npn transistors along with the higher sensitivity of lateral and substrate pnp transistors to radiation damage.
We present results and analysis investigating the effects of radiation on a variety of candidate spacecraft electronics to proton and heavy ion-induced single-event effects (SEE), proton-induced displacement damage (DD), and total ionizing dose (TID). This paper is a summary of test results.
Total ionizing dose and displacement damage testing is performed to characterize and determine the suitability of candidate electronics for NASA spacecraft and program use.
Total ionizing dose and displacement damage testing is performed to characterize and determine the feasibility of candidate electronics for NASA spacecraft and program use. AEROSPACE ENVIRONMENTS
Total ionizing dose and displacement damage testing is performed to characterize and determine the suitability of candidate electronics for NASA spacecraft and program use.
This is a Total Ionizing Dose (TID) test report for the Fujitsu Semiconductor MB85AS4MT Resistive Random Access Memory (ReRAM).
This is a Total Ionizing Dose (TID) test report for the Analog Devices AD9364 RF Transceiver.
This presentation provides information on approach to total dose radiation hardness assurance that was developed that includes variability of the space radiation environment.