Special Sensor Ultraviolet Limb Imager (SSULI)
The
Special Sensor Ultraviolet Limb Imager (SSULI) was designed and built by the
Naval Research Laboratory's Thermospheric and Ionospheric Physics Branch (Code
7623) to study the "weather" of the upper atmosphere and ionosphere
using satellite and rocket-based optical remote sensing of naturally occuring
dayglow and nightglow. NRL has developed five ultraviolet remote sensing instruments
for the Air Force Defense Meteorological Satellite Program (DMSP) . These SSULI
instruments will launch aboard the DMSP block of 5D3 satellites starting in
2000, followed by launches approximately every 18 months.
Silver
Engineering, Inc. designed portions of the SSULI Control Electronics (SCE) flight
unit. SEI designed the SCE CPU Card, the Telemetry Interface Card (TCI), the
Spacecraft Interface Card (SCI), the SEE SEM-E type Backplane, and the SCE Enclosure.
All cards utilized surface mount technology and used Field Programmable Gate
Arrays (FPGA) to reduce the number of cards and reduce power comsumption thereby
maintaining the tight weight and power budget requirements.
Silver Engineering, Inc. has particiated with the testing and simulations during
the SSULI experiments intergration and test. SEI designed and built the SSULI
Aerospace Ground Equipment (SAGE) which simulates all of the interfaces to the
SCE. SEI designed and built the SSULI Stepper Motor Driver Simulator which is
used to drive the door mechanism during calibration testing of the SSULI instrument.
SEI provided the two suite case size test units, SAGE2 and the USA Test Unit
for SSULI ground support.

SSULI
Control Electronics - SCE
Compresses
& Formats Spectrograph Data
Controls Scan Mirror, Detector Door & Dust Cover Operation
Provides All Command, Telemetry & Power Interfaces To
The DMSP SpacecraftConverts
Spacecraft Power To Secondary Power For Subsystems
Dual
Redundant DSP Architecture
FPGA's Utilized To Reduce Size & Weight
Operates On Less Than 25 Watts
Seven SEM-E Circuit Cards
CPU Card (SEI designed)
- ADSP-2100 DSP Processor, Flight Code, Actel 1020
Telemetry
Interface Card (SEI designed)
- Actel 1020, Stepper Motor Control, A/D Telemetry Acquisition,
Paraffin Actuator Control
Spacecraft
Interface Card (SEI designed)
- Actel 1020, DMSP OLS Interface Logic
Backplane
and Enclosure (SEI designed)
- SEM-E format, Single element thermal path, Weight of 9 pounds