Spacecraft Sample Collection

A special issue of Aerospace (ISSN 2226-4310). This special issue belongs to the section "Astronautics & Space Science".

Deadline for manuscript submissions: 31 July 2024 | Viewed by 581

Special Issue Editor


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Guest Editor
NASA Goddard Space Flight Center, 8800 Greenbelt Road, Greenbelt, MD 20771, USA
Interests: spacecraft; asteroid; sample collection; spacecraft instrumentation; autonomous navigation; mission design

Special Issue Information

Dear Colleagues,

On 24 September 2023, the National Aeronautics and Space Administration (NASA) successfully completed a seven-year mission to return to Earth a significant sample of the near-Earth asteroid (101955) Bennu. Also in recent years, the Japan Aerospace Exploration Agency (JAXA) and the China National Space Administration (CNSA) returned samples to Earth of the near-Earth asteroid (162173) Ryugu and the Moon, respectively. These missions are just the latest examples of successful robotic planetary sampling missions that go back more than 50 years to when the former Soviet Union returned to Earth a total of several hundred grams of lunar material during the Luna program. But missions such as these are just the start. In the near-future, even more ambitious and difficult planetary sample return missions will be attempted. For instance, in September 2023, NASA released an independent review board report regarding its Mars sample return plan. This report highlighted the tremendous technical, cost and schedule challenges of such an endeavor as well as the tremendous scientific promise. 

For this Special Issue, we invite contributions that describe lessons learned from previous robotic sample return missions as well as recent technological advances to identify, collect and return samples from locations in both the inner and outer Solar System. Submission of papers that include (but are not limited to) descriptions of  mission design, trajectories, spacecraft architecture, back planetary protection, sampling techniques and hardware, spacecraft instrumentation, Earth entry systems, sample stowage and sample archiving is encouraged.

Dr. Brent J. Bos
Guest Editor

Manuscript Submission Information

Manuscripts should be submitted online at www.mdpi.com by registering and logging in to this website. Once you are registered, click here to go to the submission form. Manuscripts can be submitted until the deadline. All submissions that pass pre-check are peer-reviewed. Accepted papers will be published continuously in the journal (as soon as accepted) and will be listed together on the special issue website. Research articles, review articles as well as short communications are invited. For planned papers, a title and short abstract (about 100 words) can be sent to the Editorial Office for announcement on this website.

Submitted manuscripts should not have been published previously, nor be under consideration for publication elsewhere (except conference proceedings papers). All manuscripts are thoroughly refereed through a single-blind peer-review process. A guide for authors and other relevant information for submission of manuscripts is available on the Instructions for Authors page. Aerospace is an international peer-reviewed open access monthly journal published by MDPI.

Please visit the Instructions for Authors page before submitting a manuscript. The Article Processing Charge (APC) for publication in this open access journal is 2400 CHF (Swiss Francs). Submitted papers should be well formatted and use good English. Authors may use MDPI's English editing service prior to publication or during author revisions.

Keywords

  • planetary sampling
  • sampling techniques and hardware
  • spacecraft instrumentation

Published Papers (1 paper)

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Research

17 pages, 7306 KiB  
Article
Instrument to Study Plume Surface Interactions (PSI) on the Lunar Surface: Science Motivation, Requirements, Instrument Overview, and Test Plans
by Ariana Bueno, Michael J. Krasowski, Norman Prokop, Lawrence C. Greer, Christina M. Adams and Nilton O. Rennó
Aerospace 2024, 11(6), 439; https://doi.org/10.3390/aerospace11060439 - 29 May 2024
Viewed by 168
Abstract
Safe landings are imperative to accomplish NASA’s Artemis goal to enable human exploration on the Moon, including sample collection missions. However, a process known as plume surface interaction (PSI) presents a significant hazard to lunar landings. PSI occurs when the engine exhaust of [...] Read more.
Safe landings are imperative to accomplish NASA’s Artemis goal to enable human exploration on the Moon, including sample collection missions. However, a process known as plume surface interaction (PSI) presents a significant hazard to lunar landings. PSI occurs when the engine exhaust of a lander interacts with the surface ejecting large amounts of regolith particles at high velocities that can interfere with the landing, disturb the surface, and damage hardware. To better understand PSI, the particle impact event (PIE) sensor is being developed to measure the kinetic energy and the flux of ejecta during landings, to quantify the potential damage, and to quantify the ejecta displaced. Multiple parameters were estimated to define the PIE instrument requirements. These estimates demonstrate that ejecta can travel at velocities of up to 800 m/s and impact the surrounding area with energies of up to 400 µJ. A significant amount of ejecta can be deposited several 10 s of meters away from the landing site, modifying the surface and causing dust-related challenges. The PIE sensor will be launched for the first time in an upcoming lunar lander. Then, PIE measurements will be used to improve PSI prediction capabilities and develop mitigation strategies to ensure safe landings. Full article
(This article belongs to the Special Issue Spacecraft Sample Collection)
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