scholarly journals Conceptual Design of a Communications Relay Satellite for a Lunar Sample Return Mission

2005 ◽  
Author(s):  
Christopher Brunner
Keyword(s):  
Conceptual Design ◽  
Lunar Sample ◽  
Sample Return ◽  
Sample Return Mission

Scientific Objectives and Payloads of the Lunar Sample Return Mission—Chang’E-5

2021 ◽  
Author(s):  
Changyi Zhou ◽  
Yingzhuo Jia ◽  
Jianzhong Liu ◽  
Huijun Li ◽  
Yu Fan ◽  
...  
Keyword(s):  
Lunar Sample ◽  
Sample Return ◽  
Sample Return Mission

scholarly journals Detailed Morphologic Mapping and Traverse Planning for a Rover-based Lunar Sample Return Mission to Schrödinger Basin

2021 ◽  
Vol 2 (4) ◽  
pp. 167
Author(s):  
Zachary R. Morse ◽  
Gordon R. Osinski ◽  
Livio L. Tornabene ◽  
Matthew Bourassa ◽  
Michael Zanetti ◽  
...  
Keyword(s):  
Lunar Sample ◽  
Sample Return ◽  
Sample Return Mission

Challenges and options for an affordable small Lunar Sample Return Mission

2006 ◽  
Author(s):  
Dr. Adam M. Baker ◽  
Andy Phipps ◽  
Martin Sweeting ◽  
Alex Ellery ◽  
Yang Gao
Keyword(s):  
Lunar Sample ◽  
Sample Return ◽  
Sample Return Mission

scholarly journals The Inner Solar System Chronology (ISOCHRON) Lunar Sample Return Mission Concept: Revealing Two Billion Years of History

2021 ◽  
Vol 2 (2) ◽  
pp. 79
Author(s):  
David S. Draper ◽  
Samuel J. Lawrence ◽  
Rachel S. Klima ◽  
Brett W. Denevi ◽  
Carolyn H. van der Bogert ◽  
...  
Keyword(s):  
Solar System ◽  
Lunar Sample ◽  
Sample Return ◽  
Sample Return Mission

scholarly journals Localization of the Chang’e-5 Lander Using Radio-Tracking and Image-Based Methods

2021 ◽  
Vol 13 (4) ◽  
pp. 590
Author(s):  
Jia Wang ◽  
Yu Zhang ◽  
Kaichang Di ◽  
Ming Chen ◽  
Jianfeng Duan ◽  
...  
Keyword(s):  
Cross Validation ◽  
Scientific Research ◽  
Radio Tracking ◽  
Lunar Sample ◽  
Sample Return ◽  
Scientific Analysis ◽  
Sample Return Mission

Chang’e-5, China’s first unmanned lunar sample-return mission, was successfully landed in Northern Oceanus Procellarum on 1 December 2020. Determining the lander location precisely and timely is critical for both engineering operations and subsequent scientific research. Localization of the lander was performed using radio-tracking and image-based methods. The lander location was determined to be (51.92°W, 43.06°N) by both methods. Other localization results were compared for cross-validation. The localization results greatly contributed to the planning of the ascender lifting off from the lander and subsequent maneuvers, and they will contribute to scientific analysis of the returned samples and in situ acquired data.

Applications of same-beam VLBI in the orbit determination of multi-spacecrafts in a lunar sample-return mission

2010 ◽  
Vol 53 (6) ◽  
pp. 1153-1161 ◽  
Author(s):  
QingHui Liu ◽  
Ming Chen ◽  
Sander Goossens ◽  
Fuyuhiko Kikuchi ◽  
Koji Matsumoto ◽  
...  
Keyword(s):  
Orbit Determination ◽  
Lunar Sample ◽  
Sample Return ◽  
Sample Return Mission

scholarly journals Research of Reinforcement Deployment Mechanism of Automatic Sampler for Lunar Sample Return Mission

2021 ◽  
Vol 781 (2) ◽  
pp. 022047
Author(s):  
Deyun Liu ◽  
Ting Zeng ◽  
Lusi Wang ◽  
Guidong Mo ◽  
Jun Li ◽  
...  
Keyword(s):  
Lunar Sample ◽  
Sample Return ◽  
Automatic Sampler ◽  
Sample Return Mission
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