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Technical report
Hiroki Senshu
Planetary Exploration Research Center, Chiba Institute of Technology
Corresponding Author
ORCiD: https://orcid.org/0000-0001-8381-666X
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This work is licensed under a CC BY 4.0 License. Read Full License
An altimeter is a critical instrument in planetary missions, for both safe operations and science activities. We present required specifications and link budget calculations for light detection and ranging (LIDAR) onboard the Martian Moons Exploration (MMX) spacecraft. During the mission phase, this LIDAR will continuously measure the distance between the spacecraft and its target. The time-series distance provides important diagnostic information for safe spacecraft operations and important information for geomorphological studies. Because MMX is a sample return mission, its LIDAR must accommodate physical disturbances on the Martian satellite surface. This resulted in changes to the optical system design.
Keywords
LIDAR, MMX, Phobos
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CURRENT STATUS: Under Review
Version (no preprint)
Posted 20 Jan, 2021
This version was not preprinted
Version 1
Posted 20 Jan, 2021
No community comments so far
Editorial decision: Major Revision
On 18 Jul, 2021
Review #2 received
Received 11 Jul, 2021
Reviewer #2 agreed
On 26 Jun, 2021
Reviews received
Received 26 Jun, 2021
Review #1 received
Received 25 Apr, 2021
Reviewer #1 agreed
On 03 Apr, 2021
Reviewers invited
Invitations sent on 01 Apr, 2021
Editor assigned
On 17 Jan, 2021
Submission checks complete
On 17 Jan, 2021
Editor invited
On 17 Jan, 2021
First submitted
On 14 Jan, 2021
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This preprint is under consideration at Earth, Planets and Space. A preprint is a preliminary version of a manuscript that has not completed peer review at a journal. Research Square does not conduct peer review prior to posting preprints. The posting of a preprint on this server should not be interpreted as an endorsement of its validity or suitability for dissemination as established information or for guiding clinical practice.
Learn more about In Review
Technical report
Hiroki Senshu
Planetary Exploration Research Center, Chiba Institute of Technology
Corresponding Author
ORCiD: https://orcid.org/0000-0001-8381-666X
Badges
Prescreen
This manuscript passed our Prescreen assessment
Complete author information
Appropriate declaration statements
Potential risks to human health
Prescreen
Peer Review Timeline
CURRENT STATUS: Under Review
Version (no preprint)
Posted 20 Jan, 2021
This version was not preprinted
Version 1
Posted 20 Jan, 2021
No community comments so far
Editorial decision: Major Revision
On 18 Jul, 2021
Review #2 received
Received 11 Jul, 2021
Reviewer #2 agreed
On 26 Jun, 2021
Reviews received
Received 26 Jun, 2021
Review #1 received
Received 25 Apr, 2021
Reviewer #1 agreed
On 03 Apr, 2021
Reviewers invited
Invitations sent on 01 Apr, 2021
Editor assigned
On 17 Jan, 2021
Submission checks complete
On 17 Jan, 2021
Editor invited
On 17 Jan, 2021
First submitted
On 14 Jan, 2021
Metrics
Comments: 0
PDF Downloads: ...
HTML Views: ...
Subject Areas
Environmental Policy
License:
This work is licensed under a CC BY 4.0 License. Read Full License
An altimeter is a critical instrument in planetary missions, for both safe operations and science activities. We present required specifications and link budget calculations for light detection and ranging (LIDAR) onboard the Martian Moons Exploration (MMX) spacecraft. During the mission phase, this LIDAR will continuously measure the distance between the spacecraft and its target. The time-series distance provides important diagnostic information for safe spacecraft operations and important information for geomorphological studies. Because MMX is a sample return mission, its LIDAR must accommodate physical disturbances on the Martian satellite surface. This resulted in changes to the optical system design.
Figure 1
Figure 2
Figure 3
This is a list of supplementary files associated with this preprint. Click to download.
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