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Systems Engineering
Provided systems engineering expertise on:- Mission/System Studies
- Instrument Feasibility
- Conceptual Design
- Trade-off Studies
- Advanced Technology Studies
- Satellite Bus and/or Payload Architectures Evaluations
- Resource Budgeting
- Requirements Definition
- Complex Interface Descriptions
- Proposal and Funding Preparation
Microbolometer
ROUTES ASTROEngineering has been contracted by the Canadian Space Agency to define a space mission for an infrared radiometer to be flown onboard a microsatellite.
NEOSSat Preliminary Design
NEOSSat
will be used in the surveillance of Near Earth Objects. ROUTES
ASTROEngineering
will provide
the preliminary design for the instrument door/baffle, power
conditioning solar panels and battery selection.THM Hyperspectral
Under three separate contracts, ROUTES ASTROEngineering has conducted 12 studies / analyses evaluating mission profiles (small satellite vs ISS), instrument design concepts, and calibration requirements for a Canadian Hyperspectral Imaging mission:- Hyperspectral
Imager Technology Assessment (CSA) (1999)
- User Requirements Analysis
- Mission Requirement Analysis
- Lumped Parameter Models – Noise Module (integrated into BOMEM models)
- On-Board Calibration Processing Unit
- Detector/Buffering Interfaces Technology Assessment
- Fore-Optics Technology for Satellite Borne Hyperspectral Imagers
- Optical Calibration Technology Assessment
- HIS On-Board Calibration System and Design Study
- Evaluation
of Technology Requirements for a Hyperspectral Mission (MDA/CSA)
(2002)
- Review of Mission Requirements
- Data Sensitivities, Instabilities and Drifts
- Hyperspectral
Phase A Studies (MDA/CSA) (2003)
- Radiometric Error Analysis and Budget
- Strategies and Preliminary Requirements for Calibration and Validation
PRISM Phase A Calibration Review
ROUTES ASTROEngineering analyzed radiometric calibration methods for PRISM, the LSPM Hyperspectral Instrument.Back to Top
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