Pulsar Fusion Advances Electric Propulsion with Hall Effect Thruster Technology

Pulsar Fusion Advances Electric Propulsion with Hall Effect Thruster Technology

Pulsar Fusion is advancing electric propulsion technology through a portfolio of Hall Effect Thrusters (HETs) designed to improve spacecraft efficiency, extend mission lifetimes and reduce operational costs. Intended for applications including attitude control, precision spacecraft control and low-thrust manoeuvres, the company's plasma thrusters utilize high specific impulse (Isp) technology to deliver greater fuel efficiency than conventional propulsion systems. This enables satellites to perform drag compensation, extend orbital lifetimes and reduce the frequency of replacement launches required to maintain space infrastructure.

The company's Hall Effect Thruster family includes three propulsion systems tailored to different mission requirements. LEOBEAR is a 500 W thruster developed for small spacecraft, Moonranger is a 5 kW system for higher-power missions and Marsranger is a 10 kW propulsion system designed for demanding in-space operations. Together, these thrusters provide scalable electric propulsion solutions across a broad range of spacecraft sizes and mission profiles.

LEOBEAR operates at 300–500 W with input voltages between 300 and 400 V, producing 12–33 mN of thrust and a specific impulse of 1300–2500 seconds. Moonranger operates between 5 and 7.5 kW, delivering 280–350 mN of thrust with a specific impulse of 1800–2010 seconds, while Marsranger operates at 5.6–10.2 kW, generating 605–690 mN of thrust and achieving a specific impulse of 2000–2200 seconds. The propulsion systems are designed to deliver progressively higher thrust while maintaining the fuel efficiency advantages associated with Hall Effect propulsion.

The thrusters are engineered with compact architectures suitable for modern spacecraft integration. LEOBEAR has an assembly mass of 2.7 kg, while Moonranger and Marsranger weigh 13.77 kg and 20.61 kg, respectively. The propulsion systems are designed to support efficient spacecraft manoeuvring while minimizing mass and volume, making them suitable for satellites operating across low Earth orbit and other in-space missions.

To ensure operational reliability, Pulsar Fusion tests its Hall Effect Thrusters at a UK government facility where the propulsion systems are evaluated for launch survivability and compliance with industry standards. By combining high specific impulse performance with rigorous qualification testing, the company aims to deliver electric propulsion systems capable of supporting long-duration missions and improving spacecraft operational efficiency.

Through its portfolio of scalable Hall Effect Thrusters, Pulsar Fusion is developing electric propulsion technologies that provide efficient in-space manoeuvring, precision orbital control and extended satellite lifetimes. The company's electric propulsion systems are designed to support commercial and institutional spacecraft operators seeking higher mission performance, lower operating costs and more sustainable long-term space operations.

About Pulsar Fusion

Pulsar Fusion is a UK-based space propulsion company specializing in electric propulsion, hybrid rocket propulsion and fusion propulsion technologies. The company develops Hall Effect Thrusters for operational spacecraft while advancing next-generation fusion-based propulsion concepts for future deep-space exploration, with a focus on efficient, scalable and sustainable in-space transportation systems.

Click here to learn more about Pulsur Fusion's Electric Propulsion

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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