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Satellite Electric Propulsion Patents: Who Leads, Trends 2026

Satellite Electric Propulsion Patents: Who Leads, Trends 2026
https://www.patsnap.com/resources/blog/rd-blog/satellite-electric-propulsion-patent-landscape/ · Patsnap · data cut-off 2026-07-31 · downloaded from the live page
Patent Landscape · Space Systems
Satellite Electric Propulsion Patents: Filing Trends and Open Claim Space
  • Filing has cooled since its 2018 peak of 22. By 2022 the midpoint year sat at just 9, and the trend has stayed flat-to-down since — a maturing claim landscape rather than a growing one.
  • F03H dominates the classification mix at 206 of 218 records. B64G spacecraft-integration claims (85) and H05H plasma-accelerator claims (22) trail far behind, marking where thruster-specific art crowds out systems-level filing.
  • The most-cited record is a 1980s-era ion thruster patent. US4838021A carries 141 citations — a reminder that citation counts here reward age and foundational claims, not current commercial relevance.
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218
Published Records
34%
Top-5 Share of All Records
-57%
Filing Growth 2021→2024
US
Leading Jurisdiction

Filing growth compares 2021 (7 records) with 2024 (3) — a three-year span. 2024 is the most recent year we treat as complete: publication lags filing by roughly 18 months, so 2025 onwards are still filling in and any growth rate that ends there would understate the field. Top-5 share is the combined record count of the five largest assignees divided by all 218 records in scope (CR5), not by the ranked leaders only.

Published byPatsnap Research··7 min readSourced from Patsnap Eureka
Overview

What the filing record shows

Satellite electric propulsion patenting concentrates almost entirely in plasma and ion propulsion claims under F03H, with spacecraft-integration filings under B64G a distant second. The search covers 218 patent families filed between 2015 and mid-2026, built around Hall thruster and ion thruster art tied to specific impulse, xenon propellant handling, erosion life and power processing units. Filing activity peaked in 2018 and has not returned to that level since, which is consistent with a field where the core thruster architectures are already well claimed.

Receiving-office data points to the United States as the primary filing venue, with Europe and China trailing, and a meaningful share of applicants also routing through the PCT system. Because publication typically lags filing by around eighteen months, the 2025-2026 figures in any trend line understate real filing activity and should be read as provisional.

Filing volume by year, 2017-2026
  1. 1ENPULSION26
  2. 2CALIFORNIA INST OF TECH14
  3. 3L 3 COMM ELECTRON TECH13
  4. 4HUGHES AIRCRAFT CO12
  5. 5SAFRAN AIRCRAFT ENGINES SAS10
  6. 6SHANGHAI INST OF SPACE PROPULSION9
  7. 7MITSUBISHI ELECTRIC CORP8
  8. 8THE BOEING CO8
  9. 9MATRA MARCONI SPACE UK7
  10. 10TECHNION RES & DEV FOUND LTD7
Source: Patsnap Eureka. Assignee ranking and totals. Derived from a Patsnap search on Satellite Electric Propulsion covering 2015–2026, data cut-off 2026-07-31. Counts reflect published records only and shift as new filings publish.Run this in Eureka MCP

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Data

Filing trend and technology composition

The two views below cover the same 218 families from different angles: one tracks filing volume over time, the other shows how those filings distribute across IPC subclasses.

A field past its filing peak

Filings rose to 22 in 2018, the high point of the window, then fell back toward single digits by the early 2020s. A 2022 midpoint of 9 confirms the decline is not a one-year dip. Readers should treat the final one or two years as undercounted given publication lag.

A field past its filing peak0613192582017222018201920202021202220232024202522026Most recent year is partial — publication lag means later filings are not yet visible.

Thruster physics, not spacecraft systems, drives the claim volume

F03H (plasma and ion propulsion) accounts for 206 of 218 records, effectively defining the corpus. B64G (spacecraft/cosmonautics integration) and H05H (plasma and particle accelerators) each capture a secondary slice, while H01J discharge-tube art and F02K reaction-propulsion claims appear only at the margins — signalling where cross-domain claims are thinner.

Thruster physics, not spacecraft systems, drives the claim volumeF03H · Plasma & ion propulsion20694.5%B64G · Cosmonautics & spacecraft8539.0%H05H · Plasma & particle accelerators2210.1%H01J · Electron & discharge tubes219.6%F02K · Jet & reaction propulsion104.6%C04B · Ceramics, cement & refractories41.8%F03G · Spring/weight & misc. motors41.8%G05F · Electric/magnetic variable con…31.4%Other156.9%

Shares are the percentage of the 218 records in scope. A patent can carry several IPC classes, so the shares add up to more than 100%.

Source: Patsnap Eureka. Filing trend and technology composition. Derived from a Patsnap search on Satellite Electric Propulsion covering 2015–2026, data cut-off 2026-07-31. Counts reflect published records only and shift as new filings publish.

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Key Patents

The most-cited prior art in this corpus

Representative filing
US20020116915A12002-08-29

Pulsed Hall Thruster System (US20020116915A1)

BUSEK COMPANY

Filed by Busek Company, this application defines a pulsed Hall thruster system combining an electron source, magnetic circuit and discharge chamber with a power processing unit and propellant delivery system, controlled to fire discrete power pulses of a duration set by a specific mathematical relationship between thruster size, propellant density and mass flow rate.The claim language ties pulse timing to a physical formula rather than a fixed value range, which affects how narrowly it can be designed around.

US20020116915A1 — patent drawing 1US20020116915A1 — patent drawing 2
View full record
Top-cited records
#Publication no.Patent titleCitations
1US4838021AElectrostatic ion thruster with improved thrust modulation141
2US5924277AIon thruster with long-lifetime ion-optics system85
3US4825646ASpacecraft with modulated thrust electrostatic ion thruster and associated method84
4US6637701B1Gimbaled ion thruster arrangement for high efficiency stationkeeping71
5US6336318B1Ion thruster having a hollow cathode assembly with an encapsulated heater, and its fabrication63
6US20020008455A1Segmented electrode hall thruster with reduced plume57
7US9194379B1Field-ionization based electrical space ion thruster using a permeable substrate47
8US6250070B1Ion thruster with ion-extraction grids having compound contour shapes47
9US5551904AMethod for making an ion thruster grid47
10US5269131ASegmented ion thruster44

Citation counts are drawn from the searched corpus only and skew toward older, foundational filings rather than recent commercial designs.

Each row carries its publication number; clicking a row searches Eureka by that number.

Source: Patsnap Eureka. Citation counts and representative records. Derived from a Patsnap search on Satellite Electric Propulsion covering 2015–2026, data cut-off 2026-07-31. Counts reflect published records only and shift as new filings publish.Run this in Eureka MCP
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Insights

Reading the numbers

Three patterns stand out once filing counts, classification spread and citation data are set side by side.

Filing momentum
22 → 9 → 2
2018 peak, 2022 midpoint, 2026 partial

The peak has passed

Filing volume dropped from a 2018 high of 22 to a 2022 midpoint of 9, with 2026 (partial) at just 2. This is a flat-or-declining trend, not a temporary dip caused by publication lag alone.

Filing trend, 2017-2026
Classification concentration
206 of 218
records classed under F03H

Thruster physics owns the claim space

F03H plasma and ion propulsion claims dominate the corpus almost completely, leaving B64G spacecraft-integration and H05H accelerator claims as much smaller secondary categories.

IPC composition
Citation skew
141 citations
US4838021A, filed pre-1990

Influence favours old art

The most-cited record in this corpus is a late-1980s ion thruster patent. High citation counts here mark foundational status, not current commercial relevance — recent filings have not had time to accumulate citations.

Most-cited records
Filing geography
87 US filings
vs. 35 EPO, 27 China, 18 WIPO

US remains the primary venue

The United States receives more than double the filings of any single alternative office, with Europe, China and PCT filings trailing at meaningfully lower volumes.

Receiving offices
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Looking for what nobody has claimed yet?

Eureka can read the same corpus for gaps instead of for coverage: under-claimed branches adjacent to satellite electric propulsion, with the prior art for and against each one.

Find the white space →
Source: Patsnap Eureka. Co-assignee relationships and derived observations. Derived from a Patsnap search on Satellite Electric Propulsion covering 2015–2026, data cut-off 2026-07-31. Counts reflect published records only and shift as new filings publish.Run this in Eureka MCP
Players

Who is filing, and where the field is thinning

Recent-year momentum data shows almost no assignee adding new filings in the latest year, which is consistent with the broader downward filing trend rather than any single company retreating from the field.

Momentum signal
-50% YoY
Shanghai Institute of Space Propulsion

Even active filers are slowing

Shanghai Institute of Space Propulsion recorded 1 filing in the latest year, down 50% year-on-year — the only assignee among the tracked group with any latest-year activity at all.

Recent-year momentum
Momentum signal
0 in latest year
ENPULSION, Boeing, Hughes, Caltech, RAFAEL

A broad filing pause among historical assignees

None of ENPULSION, Boeing, Hughes Aircraft, Caltech or the Israeli defense R&D fund show any filings in the latest tracked year, despite prior activity — pointing to a corpus dominated by legacy claims rather than active prosecution.

Recent-year momentum
Collaboration signal
5 co-assignee pairs
across the full corpus

Co-filing is rare

Only five co-assignee pairs appear across 218 families, and the strongest links trace to a single Israeli R&D fund working with named individual inventors — collaboration is the exception, not the norm, in this field.

Co-assignee pairs
🔍
Under-claimed branches worth checking before filing
These sub-areas sit outside the dense F03H core and carry comparatively thin claim coverage.
power processing unit fault tolerancehollow cathode erosion mitigationceramic discharge channel materialsgimbaled thrust vector actuationgrid erosion life extension
Rank all filers by momentum →
Recent-year filing momentum by assignee
AssigneeRecent yearYoY
Shanghai Institute of Space Propulsion1-50%
ENPULSION0
Boeing0
Hughes Aircraft Company0
California Institute of Technology (Caltech)0
Technion Research and Development Foundation Ltd.0
Safran Aircraft Engines0
Mitsubishi Electric Corporation0
Source: Patsnap Eureka. Assignee-level momentum. Derived from a Patsnap search on Satellite Electric Propulsion covering 2015–2026, data cut-off 2026-07-31. Counts reflect published records only and shift as new filings publish.Run this in Eureka MCP
What's Next

Where to take this analysis

The dataset points to specific next steps depending on whether the goal is freedom-to-operate, competitive tracking, or identifying open claim space.

Map the F03H core claim-by-claim

With 206 of 218 records classed under F03H, a granular claim map of that subclass is the highest-value next step for anyone assessing freedom to operate in Hall or ion thruster design.

Explore F03H claims in Eureka

Watch the under-claimed branches

Power processing unit fault tolerance and ceramic discharge channel materials show thinner coverage than the thruster core — worth monitoring for new entrants before the space fills in.

Track white space in Eureka

Verify current assignee activity

Recent-year momentum is near zero across most historical filers; confirming which, if any, have since resumed filing outside this window matters before drawing competitive conclusions.

Check assignee activity in Eureka
Source: Patsnap Eureka. Forward-looking reading of the same dataset. Derived from a Patsnap search on Satellite Electric Propulsion covering 2015–2026, data cut-off 2026-07-31. Counts reflect published records only and shift as new filings publish.Run this in Eureka MCP
FAQ

Common questions about satellite electric propulsion patents

Answers are grounded in the same dataset. Derived from a Patsnap search on Satellite Electric Propulsion covering 2015–2026, data cut-off 2026-07-31. Counts reflect published records only and shift as new filings publish.Run this in Eureka MCP

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Disclaimer. This page is generated from Patsnap Eureka data drawn from a limited snapshot of global patent and scientific-literature records, and is provided for general information and reference only.

Patent data carries inherent limitations: recent filings (typically the most recent 18–24 months) are under-counted due to standard publication lag; counts may be reported at either a patent-family or a patent-record basis and are not always directly comparable; classification, applicant-name, and citation data may contain errors, duplicates, or omissions; and the underlying search query defines and constrains the scope shown. As a result, the analysis may be incomplete or inaccurate and may not reflect the full technology landscape.

Nothing on this page constitutes an exhaustive prior-art, novelty, freedom-to-operate, or validity search, nor does it constitute legal, financial, investment, or professional advice, and it should not be relied upon as such. Any patent, commercial, or strategic decision should be verified independently and reviewed with qualified patent, legal, and domain professionals. Patsnap makes no warranties, express or implied, as to the accuracy, completeness, or fitness for any particular purpose of the information presented.

Machine translation. Assignee and organisation names originally recorded in Chinese, Japanese or Korean have been rendered into English by an AI translation step so that the tables stay readable. These renderings are best-effort and may not match a company’s registered English name; the original name is what the underlying patent record carries, and it is what any Eureka query launched from this page uses.

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