1U Membrane-based Deployable Solar Array Engineering Model Testing

The paper outlines the results of the development and testing of a 100 W deployable solar array for SmallSats. DEAR is a joint project between DLR, Astronika, AZUR SPACE Solar Power and ESA and aims at the development and ground demonstration of a membrane-based, deployable 100 W solar array that can be stowed in and deployed out of a 1 U CubeSat volume. In the paper the main requirements for the development will be addressed which will lead to specific design constraints. Therefore, the design is mainly driven by the required 100 W power End-of- Life, its operation in a low Earth orbit environment for at least 5 years and its tight volume and mass restrictions. Especially in terms of mass and volume constraints these requirements demand that flexible or at least semi-flexible solar arrays need to be addressed for the problem solution. The paper will give an overview on the overall system design, the functionality of the deployment process and will present the results of the environmental and functional engineering model test campaign. An overview for the further planned in-orbit demonstration missions will be presented.

Authors

Institutions

Publication Details

Published
2025-03-01
DOI
https://doi.org/10.1109/aero63441.2025.11068740
Primary Topic
Spacecraft Design and Technology
Type
article
Field-Weighted Citation Impact
0.00
Controls
|||
ALL TIME
JAN
FEB
MAR
APR
MAY
JUN
JUL
AUG
SEP
OCT
article

1U Membrane-based Deployable Solar Array Engineering Model Testing

Klaus Schneider, M. Tokarz, Tom Sproewitz, Siebo Reershemius et al.
Spacecraft Design and Technology
article

1U Membrane-based Deployable Solar Array Engineering Model Testing

Klaus Schneider, M. Tokarz, Tom Sproewitz, Siebo Reershemius, Patric Seefeldt, Tim Kubera, Sven Holz, Piotr Tochala
article en

Abstract

The paper outlines the results of the development and testing of a 100 W deployable solar array for SmallSats. DEAR is a joint project between DLR, Astronika, AZUR SPACE Solar Power and ESA and aims at the development and ground demonstration of a membrane-based, deployable 100 W solar array that can be stowed in and deployed out of a 1 U CubeSat volume. In the paper the main requirements for the development will be addressed which will lead to specific design constraints. Therefore, the design is mainly driven by the required 100 W power End-of- Life, its operation in a low Earth orbit environment for at least 5 years and its tight volume and mass restrictions. Especially in terms of mass and volume constraints these requirements demand that flexible or at least semi-flexible solar arrays need to be addressed for the problem solution. The paper will give an overview on the overall system design, the functionality of the deployment process and will present the results of the environmental and functional engineering model test campaign. An overview for the further planned in-orbit demonstration missions will be presented.

Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR) (DE), Azur Space Solar Power (DE), Astronika (Poland) (PL)
Affordable and clean energy
Openalex Percentile: Top 77%
Spacecraft Design and Technology
AI Navigator

Ask Laika to Summarize, Analyze, and Connect papers live on the map.

Summarize Papers & Methodologies

Extract key findings, datasets, and comparative methods across publications.

Benchmark Rankings & Visual Analytics

Rank top research institutions, authors, funders, topics, and journals by Field-Weighted Citation Impact (FWCI) and paper volume with instant charts.

Connect Distant Disciplines

Bridge topological clusters on the map to find hidden collaborative intersections.

1U Membrane-based Deployable Solar Array Engineering Model Testing — Klaus Schneider, M. Tokarz, et al. · (2025) | TGRS Research Map | TGRS