Revolv Space Advances Solar Array Drive Assembly Portfolio for Small Satellites

Revolv Space Advances Solar Array Drive Assembly Portfolio for Small Satellites

Revolv Space, headquartered in Torino, continues to advance the portfolio of Solar Array Drive Assemblies (SADAs) engineered specifically for small satellites and CubeSat-class missions. The company develops compact, lightweight and high-efficiency rotational mechanisms designed to optimize solar energy generation by enabling dynamic Sun-tracking capabilities in orbit. As satellite missions demand higher onboard power for advanced payloads, onboard computing and communication systems, fixed solar panels increasingly limit available energy. Revolv Space addresses this challenge with precision drive assemblies that rotate solar panels to maintain optimal orientation toward the Sun with improving energy capture and overall mission performance.

Revolv Space’s Solar Array Drive Assemblies are engineered to provide single-axis rotation for deployable solar panels, allowing spacecraft to maximize power generation throughout the orbit. The systems are designed to be compact and compatible with standardized CubeSat and small satellite platforms. The drive assemblies incorporate space-qualified motors, bearings and control electronics designed to operate reliably in vacuum, radiation and temperature extremes. By integrating rotational capability without significantly increasing mass or volume, Revolv Space enables small satellite operators to enhance power budgets while maintaining form-factor constraints.

SARA: Compact and Lightweight Solar Array Drive

SARA (Solar Array Rotation Assembly) is designed specifically for CubeSat-class platforms where volume and mass constraints are critical. The system enables deployable solar panels to rotate along a single axis, ensuring consistent Sun-pointing capability during orbital motion. SARA’s compact form factor allows integration within small satellite structures without significant redesign. The system is engineered to provide precise rotational control and efficient torque management, ensuring stable operation over extended mission lifetimes. Its lightweight design supports missions requiring enhanced power availability without compromising launch mass limitations.

HOLLY: High-Performance Solar Array Mechanism

HOLLY is developed to support higher power demands in small satellites requiring greater torque capacity and robust structural performance. The mechanism is engineered to accommodate larger or more complex solar panel configurations while maintaining efficient rotational precision. HOLLY incorporates enhanced mechanical robustness and power handling capability compared to entry-level systems. The drive assembly is designed to withstand launch loads and dynamic space conditions, offering reliable performance for satellites requiring increased energy generation for payload-intensive missions.

MARA: Modular and Scalable Solar Drive Solution

MARA is a modular Solar Array Drive Assembly designed for flexible satellite architectures. Designed to accommodate varying panel sizes and mission profiles, MARA supports scalable integration into diverse spacecraft configurations. The system emphasizes adaptability, allowing satellite manufacturers to customize panel configurations based on mission power requirements. MARA’s architecture balances mechanical strength, rotational accuracy and operational durability, ensuring compatibility with extended mission durations and evolving satellite power demands.

Revolv Space’s Solar Array Drive Assemblies are designed to operate with high positional accuracy and minimal backlash, ensuring stable Sun tracking and optimized energy capture. The systems are engineered to function reliably under radiation exposure, vacuum conditions and thermal cycling typical of Low Earth Orbit (LEO) missions. By integrating rotational drive capability into compact assemblies, the company enables small satellites to achieve higher power efficiency compared to fixed-panel configurations. This is particularly valuable for missions involving advanced communication payloads, onboard processing systems, Earth observation instruments and data-intensive applications. Revolv Space’s SARA, HOLLY and MARA assemblies provide flexible solutions that support higher power budgets without significantly increasing spacecraft size or mass. Through precision mechanical design and compatibility with standardized satellite platforms, Revolv Space contributes to improving the energy autonomy of next-generation small spacecraft.

About Revolv Space

Revolv Space is an Italian space technology company specializing in solar array drive mechanisms (SADMs) for small satellites. Headquartered in Torino, Italy, Revolv Space develops compact and lightweight rotational systems designed to maximize power generation for CubeSats and small satellite platforms. The company’s core technology focuses on enabling solar panels to dynamically track the Sun through precision rotation, increasing energy capture compared to fixed-panel configurations. Revolv Space’s drive mechanisms are engineered for high reliability, low mass and compatibility with standardized small satellite structures. By providing deployable and rotational solar solutions tailored to the small satellite market, Revolv Space supports commercial, institutional and research missions seeking enhanced onboard power efficiency and improved mission performance in Low Earth Orbit (LEO) and beyond.

Click here to learn more about Revolv Space's Solar Array Drive Mechanisms

Publisher: SatNow

GNSS Constellations - A list of all GNSS satellites by constellations

beidou

Satellite NameOrbit Date
BeiDou-3 G4Geostationary Orbit (GEO)17 May, 2023
BeiDou-3 G2Geostationary Orbit (GEO)09 Mar, 2020
Compass-IGSO7Inclined Geosynchronous Orbit (IGSO)09 Feb, 2020
BeiDou-3 M19Medium Earth Orbit (MEO)16 Dec, 2019
BeiDou-3 M20Medium Earth Orbit (MEO)16 Dec, 2019
BeiDou-3 M21Medium Earth Orbit (MEO)23 Nov, 2019
BeiDou-3 M22Medium Earth Orbit (MEO)23 Nov, 2019
BeiDou-3 I3Inclined Geosynchronous Orbit (IGSO)04 Nov, 2019
BeiDou-3 M23Medium Earth Orbit (MEO)22 Sep, 2019
BeiDou-3 M24Medium Earth Orbit (MEO)22 Sep, 2019

galileo

Satellite NameOrbit Date
GSAT0223MEO - Near-Circular05 Dec, 2021
GSAT0224MEO - Near-Circular05 Dec, 2021
GSAT0219MEO - Near-Circular25 Jul, 2018
GSAT0220MEO - Near-Circular25 Jul, 2018
GSAT0221MEO - Near-Circular25 Jul, 2018
GSAT0222MEO - Near-Circular25 Jul, 2018
GSAT0215MEO - Near-Circular12 Dec, 2017
GSAT0216MEO - Near-Circular12 Dec, 2017
GSAT0217MEO - Near-Circular12 Dec, 2017
GSAT0218MEO - Near-Circular12 Dec, 2017

glonass

Satellite NameOrbit Date
Kosmos 2569--07 Aug, 2023
Kosmos 2564--28 Nov, 2022
Kosmos 2559--10 Oct, 2022
Kosmos 2557--07 Jul, 2022
Kosmos 2547--25 Oct, 2020
Kosmos 2545--16 Mar, 2020
Kosmos 2544--11 Dec, 2019
Kosmos 2534--27 May, 2019
Kosmos 2529--03 Nov, 2018
Kosmos 2527--16 Jun, 2018

gps

Satellite NameOrbit Date
Navstar 82Medium Earth Orbit19 Jan, 2023
Navstar 81Medium Earth Orbit17 Jun, 2021
Navstar 78Medium Earth Orbit22 Aug, 2019
Navstar 77Medium Earth Orbit23 Dec, 2018
Navstar 76Medium Earth Orbit05 Feb, 2016
Navstar 75Medium Earth Orbit31 Oct, 2015
Navstar 74Medium Earth Orbit15 Jul, 2015
Navstar 73Medium Earth Orbit25 Mar, 2015
Navstar 72Medium Earth Orbit29 Oct, 2014
Navstar 71Medium Earth Orbit02 Aug, 2014

irnss

Satellite NameOrbit Date
NVS-01Geostationary Orbit (GEO)29 May, 2023
IRNSS-1IInclined Geosynchronous Orbit (IGSO)12 Apr, 2018
IRNSS-1HSub Geosynchronous Transfer Orbit (Sub-GTO)31 Aug, 2017
IRNSS-1GGeostationary Orbit (GEO)28 Apr, 2016
IRNSS-1FGeostationary Orbit (GEO)10 Mar, 2016
IRNSS-1EGeosynchronous Orbit (IGSO)20 Jan, 2016
IRNSS-1DInclined Geosynchronous Orbit (IGSO)28 Mar, 2015
IRNSS-1CGeostationary Orbit (GEO)16 Oct, 2014
IRNSS-1BInclined Geosynchronous Orbit (IGSO)04 Apr, 2014
IRNSS-1AInclined Geosynchronous Orbit (IGSO)01 Jul, 2013
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