Lunar surface traces of engine jets of Soviet sample return probes: The enigma of the Luna-23 and Luna-24 landing sites

2013 ◽  
Vol 75 ◽  
pp. 28-36 ◽  
Author(s):  
Yuriy Shkuratov ◽  
Vadym Kaydash ◽  
Xenija Sysolyatina ◽  
Alexandra Razim ◽  
Gorden Videen
Science ◽  
1968 ◽  
Vol 160 (3826) ◽  
pp. 443-444 ◽  
Author(s):  
A. L. Turkevich ◽  
E. J. Franzgrote ◽  
J. H. Patterson

Science ◽  
1970 ◽  
Vol 167 (3926) ◽  
pp. 1722-1724 ◽  
Author(s):  
A. L. Turkevich ◽  
J. H. Patterson ◽  
E. J. Franzgrote ◽  
K. P. Sowinski ◽  
T. E. Economou

2014 ◽  
Vol 101 ◽  
pp. 149-161 ◽  
Author(s):  
Myriam Lemelin ◽  
David M. Blair ◽  
Carolyn E. Roberts ◽  
Kirby D. Runyon ◽  
Daniela Nowka ◽  
...  

2021 ◽  
Author(s):  
Shingo Kameda ◽  
Masanobu Ozaki ◽  
Keigo Enya ◽  
Ryota Fuse ◽  
Toru Kouyama ◽  
...  

Abstract The JAXA’s Martian Moons Exploration (MMX) mission is planned to reveal the origin of Phobos and Deimos. Both moons will be observed by remote sensing. Sample return from Phobos will be performed. The nominal instruments were selected, including the telescopic nadir imager for geomorphology (TENGOO) and optical radiometer composed of chromatic imagers (OROCHI). The scientific objective of TENGOO is to obtain the geomorphological features of Phobos and Deimos. The spatial resolution of TENGOO is 0.3 m at an altitude of 25 km in the quasi-satellite orbit. The scientific objective of OROCHI is to obtain material distribution using spectral mapping. OROCHI is composed of seven wide-angle bandpass imagers without a filter wheel and one monochromatic imager dedicated to the observation during the landing phase. Using these two instruments, we plan to select landing sites and obtain information that supports the analysis of return samples.


Author(s):  
G. Michael Amato ◽  
James B. Garvin ◽  
I. Joseph Burt ◽  
Gabe Karpati

2017 ◽  
Vol 1 (1) ◽  
pp. 39-49
Author(s):  
Mark Darius Juszczak

The Google Lunar X Prize, which ends on December 31, 2017, has the potential to generate the first true instance of anthrocosmic media – media intended for consumption in outer space, which serves as a form of capital for an emergent autonomous field in the same. Winning the bonus segment of the X Prize consists of creating multimedia (photography or video) of one of the Apollo Landing Sites on the lunar surface. Both the terms of the creation of that media, and the media itself, are the first instances of agents acting to establish autonomy on the lunar surface – controlling how artifacts are accessed, used and represented. This paper is an exploration of the conditions required for the emergence of an anthrocosmic media age – an age where agents use media as a form of power in outer space to establish autonomy in fields that are also in outer space.


1968 ◽  
Vol 73 (24) ◽  
pp. 7621-7629 ◽  
Author(s):  
Everett D. Jackson ◽  
Howard G. Wilshire

Author(s):  
Z. Bo ◽  
W. Wan ◽  
C. Liu ◽  
K. Di ◽  
Z. Liu ◽  
...  

Abstract. In the lunar surface sampling mission, the drop operation that transferring the packaging container into the sample return container is a vital step. In this paper, for supporting the drop operation, we proposed a method to measure the coaxiality between the two containers based on the monocular vision pose measurement using ellipse and line features. The method first extracts ellipse and line features in the 2D image to calculate the initial parameters. Then, the initial parameters and the point set are used to fit the curve by the cylinder perspective contours fitting method, where the constraints between ellipse and line features are used to improve the robustness to varying noises. Next, given the fitting ellipse and camera parameters, the pose of the packaging container is solved by using circle-based method. Finally, the coaxiality of the two containers is calculated based on the relative pose between them. Simulation experiments were carried out and the results show the effectiveness and reliability of the proposed method.


1968 ◽  
Vol 1 ◽  
pp. 462-470
Author(s):  
Israel Taback

The U.S. Lunar Orbiter Spacecraft Program was conceived to search out potential Apollo landing sites, and to return detailed photographic coverage of the lunar surface for scientific study. The first flight was launched in August 1966, and the successful launch of the fifth orbiter was in August 1967. All five were successful and returned to Earth a large amount of photographic data.Presented in this paper is a short description of the spacecraft system with particular emphasis on the photographic system. The intent is to supply information which will permit a better understanding of the photographic data to be presented by Dr. William Brunk in the following paper.


2020 ◽  
Author(s):  
Nick Gollins ◽  
Shahrzad Timman ◽  
Max Braun ◽  
Markus Landgraf

<div> <p>In the context of an accelerated lunar exploration agenda on international level, ESA is engaging in studies to enable European roles in the near and mid-term which can support the international community. While near-term opportunities exist in “boots-on-the-ground” human lunar return in the frame of the NASA Artemis programme and commercial (CLPS) robotic landers, ESA continues to prepare the next step in sustainability with the European Large Logistic Lander (EL3).</p> <p>Returning to the Moon not only yields fundamentally important science opportunities for our understanding of the Solar System but also allows us to test hardware and operational procedures for the exploration and utilization of space beyond Low Earth Orbit (LEO). EL3 will be a sustainable programme that will allow a diversity of missions for the science community. Whilst EL3 is intended to be a generalised lander capable of delivering a wide variety of cargo, such as science experiments, crew supplies, or unpressurised rovers, the most studied mission to date is a sample return package comprised of a return stage and a rover. EL3 Sample Return will land on the lunar surface, demonstrate surface operations, and return ∼15 kg of samples to the lunar Gateway and back to Earth by the astronauts aboard Orion. Hence, the mission will begin a robotic pathway toward sustainable human exploration of the Moon and beyond. </p> <p>To achieve this, some of the key objectives include: (1) Create opportunities for science, particularly sample return, which has been highlighted as a key aspect of ESA’s lunar science strategy; (2) Gain scientific and exploration knowledge by scouting for potential resources; (3) Create opportunities to demonstrate and test technologies and operational procedures for future Mars missions; (4) Preparing for more sustainable human lunar missions by implementing, demonstrating, and certifying technology elements for vehicle reusability, mobility, and night survival.</p> <p>EL3 Sample Return will consist of the EL3 cargo lander, an interface element housing a 330 kg rover, and a Lunar Ascent Element (LAE) that will return the samples to the lunar Gateway. The rover will be designed for driving more than 100 km at relatively high speed and surviving the lunar night. Whilst mostly operated by ground control on Earth, the rover could also be partly tele-operated by astronauts aboard the Gateway. Once landed on the lunar surface, the rover will immediately collect a contingency sample and will then collect additional samples along a ∼35 km long traverse. The rover will carry a suite of scientific instruments that will allow the comprehensive study of the sampling locations, providing the context of the samples, as well as the geology along the traverse. After depositing the samples into the LAE, the rover will embark on a 100+ km traverse along which it will take further in-situ measurements over the course of a year or more.</p> <p>In summary, the goals of the EL3 programme will be to support international crewed lunar activities, develop and fly the technologies necessary to build Europe’s lunar capability, and serve the needs of the lunar science community.</p> </div><p> </p>


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