Phase Four Next Generation Max-V Engine to use Domestically Sourced Iodine-Based Propellant

Phase Four Next Generation Max-V Engine to use Domestically Sourced Iodine-Based Propellant

Phase Four, the creator of the radio-frequency thruster for satellite propulsion, has announced that it will expand its Maxwell turn-key plasma propulsion line and offer satellite manufacturers an industry-first high-performance engine using an inexpensive, domestically sourced iodine-based propellant. Max-V leverages the Maxwell Block 2 engine's innovative architecture and builds on the radio-frequency thruster's propellant-agnostic capabilities.

"Legacy electric propulsion systems are tied to noble gases like xenon and krypton," said Phase Four CEO, Beau Jarvis. "These noble gases, while high performing, are largely sourced outside of the United States in China, Russia and Ukraine. The US has no real control over this supply chain, which is subject to high price volatility and recent severe supply issues." Phase Four board member, former NASA Administrator Jim Bridenstine observed, "This year we've seen xenon prices spike to over $30,000 per kilogram. This is cost prohibitive for both commercial and government satellite constellations in low Earth orbit." Bridenstine continued, "The US is the world's third largest iodine producer, and my home state of Oklahoma leads the way in domestic production. With Max-V, we can ensure a fully domestic supply chain and readily accessible low-cost propellant."

Phase Four's Maxwell Block 1 engine gained flight heritage in early 2021. Maxwell Block 2 engine deliveries began earlier this year. With double-digit commercial flight units delivered, the company is now focusing on its Max-V development effort. Maxwell's new chassis-style design enables rapid on-ramping of improvements in the core areas of the thruster, power electronics, and propellant subsystems. This architecture is streamlining the Max-V development process as is the company's significant experience with iodine-based propellants through its recent U.S. Air Force AFWERX award.

"Maxwell's new modular chassis architecture enables us to introduce improved capabilities within the same form factor," said Phase Four CTO, Umair Siddiqui. "Using an iodine-based propellant instead of a noble gas propellant stored at very high pressure provides a number of benefits to our customers. Iodine stores as a solid without high-pressure valves or vessels, which means we can deliver fully fueled engines directly to our customers." Siddiqui continued, "Iodine also stores about three times more densely than xenon, which means our propulsion systems will offer much higher total impulse in the same unit volume as legacy electric propulsion systems."

Phase Four's RF Thruster firing using Max-V's new iodine-based propellant"We've always said that Phase Four delivers game-changing propulsion systems, and Max-V will do just that," said Phase Four CEO, Beau Jarvis. "We are building a product that will dramatically lower costs and extend operational lifetimes of small satellites in low Earth orbit and provide a significantly higher total impulse for missions beyond LEO."

Max-V is anticipated to be available for order in the second half of 2023. The system is designed to operate from 200 Watts to 1.5 kiloWatts, achieve 50 mN thrust, over 1,200 s Isp and deliver over 100 kNs total impulse. Max-V's iodine-based propellant will cost under $400 per kilogram and be incorporated into the purchase price. Max-V's form factor is similar to Phase Four's current Maxwell Block 2 engine. The system will ship fully fueled, ready for installation, and will require no ground fueling operations prior to launch.

Click here to learn about various RF Ion Thrusters from Phase Four.

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