Satellite Electric Propulsion Patents: Who Leads, Trends 2026
- 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.
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.
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.
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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.
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.
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%.
Go deeper on Satellite Electric Propulsion with Eureka
This page is one run against one query. Ask Eureka your own question about satellite electric propulsion and every answer comes back with the patent numbers behind it.
Try EurekaThe most-cited prior art in this corpus
Pulsed Hall Thruster System (US20020116915A1)
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.


| # | Publication no. | Patent title | Citations |
|---|---|---|---|
| 1 | US4838021A | Electrostatic ion thruster with improved thrust modulation | 141 |
| 2 | US5924277A | Ion thruster with long-lifetime ion-optics system | 85 |
| 3 | US4825646A | Spacecraft with modulated thrust electrostatic ion thruster and associated method | 84 |
| 4 | US6637701B1 | Gimbaled ion thruster arrangement for high efficiency stationkeeping | 71 |
| 5 | US6336318B1 | Ion thruster having a hollow cathode assembly with an encapsulated heater, and its fabrication | 63 |
| 6 | US20020008455A1 | Segmented electrode hall thruster with reduced plume | 57 |
| 7 | US9194379B1 | Field-ionization based electrical space ion thruster using a permeable substrate | 47 |
| 8 | US6250070B1 | Ion thruster with ion-extraction grids having compound contour shapes | 47 |
| 9 | US5551904A | Method for making an ion thruster grid | 47 |
| 10 | US5269131A | Segmented ion thruster | 44 |
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.
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Three patterns stand out once filing counts, classification spread and citation data are set side by side.
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.
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.
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.
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.
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.
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.
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.
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.
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.
| Assignee | Recent year | YoY |
|---|---|---|
| Shanghai Institute of Space Propulsion | 1 | -50% |
| ENPULSION | 0 | — |
| Boeing | 0 | — |
| Hughes Aircraft Company | 0 | — |
| California Institute of Technology (Caltech) | 0 | — |
| Technion Research and Development Foundation Ltd. | 0 | — |
| Safran Aircraft Engines | 0 | — |
| Mitsubishi Electric Corporation | 0 | — |
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 EurekaWatch 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 EurekaVerify 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 EurekaCommon questions about satellite electric propulsion patents
The corpus of 218 families shows filing concentrated among a small group of aerospace and research organisations, including Boeing, Hughes Aircraft, Caltech and Shanghai Institute of Space Propulsion, alongside newer entrants like ENPULSION. However, recent-year momentum data shows almost none of these organisations filing new applications in the latest tracked year, so historical leadership does not necessarily reflect current activity. Anyone assessing competitive position should check whether a given assignee has filed outside this specific search window before treating them as currently active.
Filing peaked at 22 in 2018 and fell to a midpoint of 9 by 2022, with the partial 2026 figure at just 2. This pattern is consistent with a field where core Hall thruster and ion thruster architectures were claimed relatively early, leaving less unclaimed ground for new filings. It is worth noting that publication lags filing by roughly eighteen months, so the very latest years in any trend understate true filing activity, but the decline visible through 2022-2023 predates that lag effect and reflects a genuine slowdown.
Both fall under the F03H plasma and ion propulsion classification that accounts for 206 of the 218 records in this dataset, and the search terms for both appear together in most of the underlying claims. Hall thruster patents typically emphasize the magnetic circuit and discharge chamber design, as seen in filings like the pulsed Hall thruster system from Busek Company, while ion thruster patents more often focus on ion-optics systems and electrostatic grid design. In practice the two technologies share enough claim language — around specific impulse, xenon propellant handling and erosion life — that a freedom-to-operate search should cover both together.
The most-cited record, US4838021A, covers an electrostatic ion thruster with improved thrust modulation and carries 141 citations within this corpus, making it the single most-referenced document in the dataset. High citation counts in a searched patent corpus tend to reward older, foundational filings simply because they have had decades to accumulate references, not because the underlying technology remains commercially central today. Readers should treat this and similarly old top-cited records as markers of historical influence on subsequent claim drafting, rather than as evidence of current market relevance.
The classification data shows F03H claims heavily saturated at 206 of 218 records, while adjacent areas such as power processing unit fault tolerance, ceramic discharge channel materials, and gimbaled thrust vector actuation carry comparatively thinner coverage. Co-assignee data also shows collaboration is rare, with only five co-filing pairs across the entire corpus, suggesting most work happens within single organisations rather than joint ventures that might otherwise crowd a sub-area. Anyone looking to file new claims should start by checking these thinner branches rather than the dense F03H core, where a decades-old foundational patent base already occupies much of the obvious claim territory.
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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.