logo_ua
Desktop EN 2023
logo_ua
logo_ua

7. Autonomous deployable landing interface: a detailed technical framework for Mitigating terminal descent risks on planetary surfaces

Date of receipt of the article for publication: 03.11.2025

Date of acceptance of the article for publication after review: 17.11.2025

Date of publication: 27.01.2026

e-ISSN: 2617-5533

Автори: Iteba A. K., Weramundi N. E.

Organization: University of Nairobi

Page: Kosm. teh. Raket. vooruž. 2025 (2); 67-70

DOI: https://doi.org/10.33136/stma2025.02.067

Language: English

Annotation: The terminal descent phase of landing is a mission-critical failure point for all planetary surface exploration. This paper presents a detailed technical framework for the Lunar Landing Interface (LLI), a deployable, autonomous ground structure designed to create a controlled environment that mitigates these universal risks. We provide an in-depth analysis of the material science, component design, and operational principles of the LLI. Specifi c focus is given to the proposed solutions for electromagnetic compatibility (EMC); the power nfrastructure required for high-voltage electrostatic systems; the system’s structural and mechanical reliability through the use of solid-state actuators and robust materials; and the strategic costbenefi t of lander mass reduction enabled by this infrastructure. The scientifi c novelty of this work lies in the integrated systems approach, combining origami-inspired deployment with active dust mitigation and ground-based autonomous guidance to solve the terminal descent problem holistically. The practical signifi cance is a clear path toward reducing the cost and increasing the safety of lunar access, thereby enabling a sustainable lunar economy. This work expands upon a preliminary concept to provide the detailed theoretical and engineering rationale necessary to prove the LLI’s feasibility and justify further investment in its development, directly addressing reviewer feedback

Key words: Lunar Landing, Terminal Descent, Dust Mitigation, Origami Structures, Autonomous Systems, Spacecraft Design, Regolith, ShapeMemory Alloys

Bibliography:

1. Mike Wall. Intuitive machines’ private athena probe lands near lunar south pole – but it may have tipped over, 20.
2. NASA Science. Beresheet, 2019.
3. KYODO NEWS. Japan ispace fails in bid for 1 st moon landing by asian private firm, 2025.
4. Thornton Bryce, Ireland Tom. The economics of reusable launch vechicles. New Space. 10(2). 125-135, 2022.
5. Attard M., Chirima G., Kar-Eng K. A review of the applications of indium tin oxide (ito). Journal of Physics: Conference Series, 2071:012001, 2021.
6. Shaw J.A., Grummon D.S., Folias S. Shape memory alloy applications in aerospace. Progress in Aerospace Sciences, 126:100743, 2021.
7. Sternovsky Z., Szalay J.R., Horányi M., Drake E. Photoelectric charding and transport of lunar dust. Journal of Geophysical Research: Planets. 128 (5), 2023.

Downloads: 20
Abstract views: 
273
0 citations in OpenAlex database (as of 04.03.2026 13:30)
0 citations in Scopus database (as of 13.03.2026 23:49)
0 citations in Zenodo database (as of 13.03.2026 23:49)
Dynamics of article downloads
Dynamics of abstract views
Downloads geography
CountryCityDownloads
USA Ashburn; El Monte; Ashburn; Ashburn; San Mateo; San Mateo; Pompano Beach; Lakeside; Lakeside; San Francisco; Albany; Albany12
France Roubaix; Paris2
Unknown Hong Kong; Hong Kong2
Ukraine Dnipro; Kremenchuk2
China1
Iran Tehran1
Збірник науково-технічних статей


Збірник науково-технічних статей


Збірник науково-технічних статей


Збірник науково-технічних статей


Scopus - Yuzhnoye State Design Office publications


OpenAlex - Yuzhnoye State Design Office publications


Zenodo - Yuzhnoye State Design Office publications


ROAR - Yuzhnoye State Design Office repository record


ROR - Yuzhnoye State Design Office organization ID


Open Archives - Validate Site

Keywords cloud

Visits:273