Laser Technology in Photonic Applications for Space
Abstract
:1. Introduction
2. Laser Devices
2.1. Semiconductor Lasers
2.1.1. Edge-Emitting Laser (EEL)
2.1.2. Vertical-Cavity Surface-Emitting Laser (VCSEL)
2.2. Solid State Laser (SSL)
2.3. Fiber Lasers
2.4. Other Types of Laser Sources
3. Lasers in Space
3.1. Science
3.1.1. Remote Sensing (LIDAR)
- Earth Observation
- Other Solar System Targets
3.1.2. Spectroscopy
3.1.3. Quantum Scientific Technologies
3.2. Communication
- almost limitless bandwidth thanks to the wavelength range available,
- lightweight and low volume,
- mechanical flexibility,
- galvanic isolation,
- propagation to longer distances thanks to the reduced divergence.
3.2.1. Space-Earth
3.2.2. Space-Space
- Intra-Satellite Communication
- Inter-Satellite Communication
3.2.3. Quantum Communication
3.3. Fiber Optic Sensing
3.4. Optopyrotechnics in Propulsion
- Indirect Ignition System by Detonation of Pyrotechnics Using Short Laser Pulses
- Direct Laser Ignition
3.5. Integrated Solid State Gyroscopes
4. Technical Specs and Rrequirements
- reliable for several operational years (commonly 10–20 years),
- usual operation and non-operational temperatures between ≤−45 °C to ≥+85 °C; although those vary depending on the mission space target (Figure 4), or different objects with more or less proximity to the sun [132], tenths of cycles between minimum and maximum limits have to be performed on materials and devices for them to be qualified,
- harsh vibration (Table 1) and shock (usually 1500 g) resistance, conditions normally due to launch take off and possible planetary landing,
- vacuum compatibility (10−9 torr),
- no contamination. Low out-gassing, in terms of total mass loss (TML) and collected volatile condensable materials (CVCM) <0.1%.
5. Difficulties, Drawbacks—But Also Final Advantages
- almost limitless bandwidth for lasercom devices,
- immunity to electromagnetic waves,
- reliability,
- efficient and low power consumption,
- small form factor,
- low weight.
6. Conclusions
- assessment of space suitability of commercially available laser products through functional and environmental testing,
- selection of the most suited component and collaboration with its manufacturer for improvement towards space qualification,
- formal space qualification of the resulting device.
Author Contributions
Funding
Acknowledgments
Conflicts of Interest
References
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Frequency (Hz) | Level |
---|---|
20 | 0.052 g2/Hz |
20–50 | +6 dB/octave |
50–800 | 0.32 g2/Hz |
800–2000 | −6 dB/octave |
2000 | 0.052 g2/Hz |
Overall | 20.0 grms |
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Guilhot, D.; Ribes-Pleguezuelo, P. Laser Technology in Photonic Applications for Space. Instruments 2019, 3, 50. https://doi.org/10.3390/instruments3030050
Guilhot D, Ribes-Pleguezuelo P. Laser Technology in Photonic Applications for Space. Instruments. 2019; 3(3):50. https://doi.org/10.3390/instruments3030050
Chicago/Turabian StyleGuilhot, Denis, and Pol Ribes-Pleguezuelo. 2019. "Laser Technology in Photonic Applications for Space" Instruments 3, no. 3: 50. https://doi.org/10.3390/instruments3030050