The benefits of very low earth orbit for earth observation missions
@article{Crisp2020TheBO, title={The benefits of very low earth orbit for earth observation missions}, author={Nicholas H. Crisp and Peter C. E. Roberts and Sabrina Livadiotti and Vitor Toshiyuki Abrao Oiko and Steve Edmondson and Sarah J. Haigh and Claire Huyton and Luciana A. Sinpetru and K. L. Smith and Stephen D. Worrall and Jonathan Becedas and R. M. Dom'inguez and D. J. Gonz'alez and Virginia Hanessian and Anders M{\o}lgaard and J. Nielsen and Morten Bisgaard and Y.-A. Chan and Stefanos Fasoulas and Georg H. Herdrich and Francesco Roman{\`o} and C. Traub and D. Garc'ia-Alminana and S. Rodr'iguez-Donaire and Miquel Sureda and D. O. Kataria and R. B. Outlaw and B. Belkouchi and Alexis Conte and J. S. Perez and Rachel Villain and Barbara Heisserer and Ameli Schwalber}, journal={Progress in Aerospace Sciences}, year={2020} }
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References
SHOWING 1-10 OF 177 REFERENCES
Very Low Earth Orbit mission concepts for Earth Observation: Benefits and challenges.
- Physics
- 2014
Very Low Earth Orbits (VLEO) can be defined as the orbits with a mean altitude below 450 km. Operating in these orbits can provide a number of benefits to Earth observation spacecraft as the…
Descending Sun-Synchronous Orbits with Aerodynamic Inclination Correction
- Physics, Geology
- 2015
Earth observation spacecraft use sun-synchronous orbits because they enable observations of ground targets with similar illumination conditions over different passes. To achieve these orbits,…
Moderately Elliptical Very Low Orbits (MEVLOs) as a Long-Term Solution to Orbital Debris
- Physics
- 2012
Long-term orbital debris is a continually growing problem that has proven challenging to overcome. A straightforward solution to the problem is to put the majority of future LEO spacecraft into…
Aerodynamic Stability for CubeSats at ISS Orbit
- Physics
- 2013
At altitudes below 500 km, satellites experience a significant amount of aerodynamic drag that can be utilized to stabilize satellites to align with the relative wind direction. Designing a…
DISCOVERER: Radical Redesign of Earth Observation Satellites for Sustained Operation at Significantly Lower Altitudes
- Environmental Science
- 2017
The DISCOVERER project aims to radically redesign Earth observation satellites for sustained operation at significantly lower altitudes by carrying out foundational research in the aerodynamic characterisation of materials, in atmosphere-breathing electric propulsion for drag-compensation, and in active aerodynamic control methods.
Quantifying the Cost Reduction Potential for Earth Observation Satellites
- Business
- 2017
In the present budget environment, there is a strong need to dramatically drive down the cost of space missions. There is the perception that SmallSats are inherently much lower cost than more…
RAM Electric Propulsion for Low Earth Orbit Operation: an ESA study.
- Physics
- 2007
This paper summarizes the results of the RAM-EP system concept study. The study involved the investigation of the feasibility of using electric propulsion together with gas collected from the…
Orbital Debris and Sustainability of Space Operations 46
- Physics, Geology
- 2013
The orbital particle environment around the Earth is dominated by man-made space objects, except for a limited particle size regime below 1 mm, where meteoroids provide a significant contribution, or…
Aerodynamics of Satellites on a Super Low Earth Orbit
- Physics
- 2009
The Super Low Altitude Test Satellite is an engineering test satellite currently under development in Japan Aerospace Exploration Agency in an attempt to open a new frontier of space utilization on…