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Home | NASA Final Report Cover | Table of Contents | SCM Flight Prototype Specifications
Part 4: SCM Flight Prototype Specifications

Figure 4.0.01: The flight-qualified SCM weighs 650 grams (<1½ pounds)
Size: 6.5"x 3.75"x 2.75"
Mass: 650 grams
Temperature range:
- Store at: -55°C to 105°C
- Expanded operating range: -24°C to +61°C
- Calibrated operating range: -24°C to 40°C
Power Requirement: Less than 2Watts, 28V (unregulated)
Vibration Tolerance: 14.5 G's (rms) for 3 minutes each orthogonal axis
Radiation Tolerance: Estimated at 50kRads based on components used
EMI: Only preliminary data available. SCM does not produce noticeable EMI
S/C Floating Potential Range: -145 to +45 volts with 0.1 volt precision
Interface: RS422 two-wire differential
Interface Connector: DB-9 (pins 1-5 and 8)
Thermal Control: S/C supplies thermal via to SCM chassis
Table of Contents (+/-)
- Project Objectives
- Development of the SCM
- Tests of the SCM
- Goembel Instruments Functional Tests
- NASA/KSC Advanced Functional Test
- Vibration Tests
- Thermal-Vacuum Tests
- Preliminary EMI Tests
- Comment on SCM Tests
- SCM Flight Prototype Specifications
- Potential Applications
- References
- Footnotes
Report Documentation Page (Form 298)