Mechanical Environment | Temperature | Operational Life | Radiation | Other | ||
---|---|---|---|---|---|---|

Low Earth Orbit (LEO) | Geosynchronous Orbit (GEO) | Highly Elliptical (HEO) Deep Space | ||||

Sine Vibration | Operational | On Orbit | Total Dose | Total Dose | Total Dose | EMI / EMC |

The qualification level sine vibration shall be 16g for the frequency range 5-100 Hz with displacement limited to 1.0 inch peak to peak. | -20 degree F to +50 degree F (controlled mounting temperature) | 10 Flights over 10 years. | 1 Krad Total Dose. | 100 - 300 Krad Total Dose. | 100 Krad - 1Mrad Total Dose. | MIL-STD-461C |

Random Vibration | Non-Operational | Ground Test | Single Event Latchup/Burnout | Single Event Latchup/Burnout | Single Event Latchup/Burnout | Reliability |

"7.7 gRMS 10 to 40 Hz - Constant 0.022 g2/hz 40 to 70 Hz - Plus 6 dB/octave to .067 g2/hz 70 to 200 Hz - Constant 0.067 g2/hz 200 to 250 Hz - Minus 6 dB/octave to 0.043 g2/hz 250 to 900 - Constant .043 g2/hz 900 to 2000 - Minus dB to .04 g2/Hz" |
-55 degree C to +125 degree C | Cumulative operation of 75 months. | Immune to linear energy transfer (LET) of 14 MeV/cm2/mg as demonstrated by when exposed to a minimum of 200 Mega electron Volts (MeV) (+/- 10 MeV) protons to a fluence of 1010 protons/cm2. | Immune to linear energy transfer (LET) of 36 MeV/cm2/mg | Immune to linear energy transfer (LET) of 36 to 62 MeV/cm2/mg | MTBF of 20,000 Hours. |

SOURCE: Sources