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Space & Orbital Computing

2026-11-05
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Applications · Space & Orbital Computing

Space Orbital Data Center JONSN Micro Gear Pump Zero-Leakage Thermal Control Solution

As artificial intelligence computing demand continues to spill over, deploying data centres in low Earth orbit (LEO) is moving from concept toward engineering practice. Orbital data centres, computing constellations and on-board edge nodes leverage the near-unlimited solar energy and the natural deep-space cold background of space to carry high-density compute at a lower PUE.

Space & Orbital Computing

Magnetic Zero Leakage

The pump cavity and motor are isolated by static sealing, with torque transmitted non-contact by magnetic force, completely eliminating rotating dynamic seals. The entire fluid path has no channel to leak to the environment, and the working fluid is strictly sealed inside the loop — eliminating the space leakage risk at mechanism level.

Flow Accuracy ±0.5%

As a positive displacement pump, output flow is linearly determined by rotational speed and is stably supplied within ±0.5% accuracy. Regardless of how cold plate back-pressure varies, flow does not drift with load, making the heat transfer capability of every compute board predictable and simulatable.

Pulsation ≤1%

The continuous volume change of gear meshing keeps flow pulsation controlled to ≤1%, producing a uniform cold plate temperature field and small chip junction temperature ripple — particularly suited to advanced packaging and high-bandwidth memory that are sensitive to thermal gradients.

Maintenance-Free ≥20,000 h

No dynamic seals, no consumable soft tubing, combined with low-wear gear pairs and long-life bearings, the maintenance-free operating life is designed at ≥20,000 hours, matching the on-orbit mission duration with no personnel intervention required.

Introduction: The Orbital Compute Era, Thermal Management as the First Constraint

As artificial intelligence computing demand continues to spill over, deploying data centres in low Earth orbit (LEO) is moving from concept toward engineering practice. Orbital data centres, computing constellations and on-board edge nodes leverage the near-unlimited solar energy and the natural deep-space cold background of space to carry high-density compute at a lower PUE. But the reverse side of the orbital environment is equally severe: microgravity, high vacuum, strong radiation, severe temperature cycling, and the iron rule that nothing can be serviced after launch — every component's reliability is magnified under inspection.

In high-density compute scenarios, the heat dissipation of a single high-compute chip has already reached the hundred-watt level; air cooling fails in vacuum and microgravity, making liquid cooling the only viable thermal management path. And the "heart" of the liquid cooling loop — the circulation pump — must run unattended for long periods under zero leakage, high precision and long service life. This is exactly where JONSN micro magnetic gear pumps enter orbital computing infrastructure.

Deficiencies of Conventional Pumps in Space Liquid Cooling

Conventional industrial pumps perform well on the ground, but once they enter a space liquid cooling loop, their inherent shortcomings are significantly amplified:

Deficiency 01
Dynamic Seal Leakage Risk
Centrifugal pumps, diaphragm pumps and similar units generally use rotating shaft dynamic seals. In microgravity and high vacuum, once the sealing interface fails, leakage of the working fluid (deionised water, electronic fluorinated liquid or ammonia) will contaminate the payload, induce short circuits, and may even jeopardise the safety of the entire platform.
Deficiency 02
Large Flow Pulsation, Uneven Heat Transfer
Peristaltic pumps rely on rollers squeezing soft tubing, with pulsation rates commonly reaching 10%–30%. This causes temperature fluctuation across cold plate surfaces and oscillation of chip junction temperature, which is detrimental to the stable operation of high heat flux density devices.
Deficiency 03
Bulky and Heavy, High Launch Cost
Conventional pumps are mostly redundantly designed for ground installation, with excessive volume and mass. Under launch costs priced per kilogram, every 100 g removed is engineering-meaningful.
Deficiency 04
Weak Radiation and Thermal Cycling Capability
Ordinary motor windings, electronic drivers and sealing materials age easily under cumulative total ionizing dose (TID) and hot-cold alternation, failing to meet multi-year on-orbit mission durations.
Deficiency 05
Many Wear Parts, No On-Orbit Maintainability
Mechanical seals, bearings and other consumables can be replaced periodically on the ground, but in space they are one-time components — life equals system life.
Deficiency 06
High Energy Consumption
In the limited power budget of a satellite, pump power consumption directly encroaches on the available power for the compute load; an inefficient pump is equivalent to reduced compute output.

JONSN Micro Gear Pump Advantages

JONSN micro magnetic gear pumps are built around "positive displacement + magnetically coupled full enclosure" and systematically optimised against the key constraints of space liquid cooling. The advantages can be summarised in six points:

Advantage 01
Magnetic Zero Leakage
The pump cavity and motor are isolated by static sealing, with torque transmitted non-contact by magnetic force, completely eliminating rotating dynamic seals. The entire fluid path has no channel to leak to the environment, and the working fluid is strictly sealed inside the loop — eliminating the space leakage risk at mechanism level.
Advantage 02
High-Precision Constant Flow
As a positive displacement pump, output flow is linearly determined by rotational speed and is stably supplied within ±0.5% accuracy. Regardless of how cold plate back-pressure varies, flow does not drift with load, making the heat transfer capability of every compute board predictable and simulatable.
Advantage 03
Low Pulsation, Smooth Transport
The continuous volume change of gear meshing keeps flow pulsation controlled to ≤1%, producing a uniform cold plate temperature field and small chip junction temperature ripple — particularly suited to advanced packaging and high-bandwidth memory that are sensitive to thermal gradients.
Advantage 04
Compact and Lightweight
The miniaturised structure keeps the mass of a single pump below 500 g, allowing direct integration into on-board cold plates or loop manifolds, maximising savings in launch mass and cabin volume.
Advantage 05
Wide Temperature Range and Media Compatibility
The pump body uses a combination of space-grade materials — stainless steel, PEEK and ceramic — compatible with mainstream aerospace working fluids including deionised water, water-glycol, electronic fluorinated liquid and ammonia. The operating temperature covers -40 °C to +120 °C, adapting to the launch phase and on-orbit thermal cycling.
Advantage 06
Long Life, Maintenance-Free
No dynamic seals, no consumable soft tubing, combined with low-wear gear pairs and long-life bearings, the maintenance-free operating life is designed at ≥20,000 hours, matching the on-orbit mission duration with no personnel intervention required.

Parameter Validation and Application Cases

Core Parameters (JONSN-MPG Series)

ItemSpecification
Rated Flow100 mL/min
Maximum Outlet Pressure10 bar
Flow Accuracy±0.5%
Flow Pulsation≤1%
Sealing FormMagnetically coupled full enclosure (zero leakage)
Compatible MediaDeionised water, water-glycol, electronic fluorinated liquid, ammonia, etc.
Operating Temperature Range-40 °C ~ +120 °C (pump body)
Drive Voltage12 / 24 VDC (customisable)
Rated Power Consumption≤15 W
Unit Mass≤480 g
Design Life≥20,000 h (maintenance-free)
Interface FormCompression fitting / quick-connect (customisable)

Space-&-Orbital-Computing1.webp

Validation Testing

JONSN-MPG series must pass a set of on-orbit-environment reliability validations before entering space applications:

01
Thermal Vacuum Cycling
In 10⁻³ Pa vacuum with -40 °C ~ +85 °C alternating conditions, 100 cycles are completed with no leakage throughout and performance degradation < 3%.
02
Random Vibration
Covering the launch-phase vibration spectrum of 5–2000 Hz with a total RMS acceleration of 14.1 grms; functions normal and no structural loosening after testing.
03
Radiation Tolerance
The standard version withstands a certain total ionizing dose (TID); radiation-hardened driver and electronics options are available for long-duration LEO missions to meet the mission dose budget.

Application Case (Representative Illustration)

A 12U on-board edge computing module from a commercial aerospace enterprise integrates 3 high-compute SoCs, with a per-board heat dissipation of approximately 180 W. Its single-phase liquid cooling loop uses a JONSN-MPG micro gear pump to circulate electronic fluorinated liquid stably at 100 mL/min, holding chip junction temperature below 65 °C. After orbit insertion, the module has been running continuously for more than 14 months with no pump failure and no performance degradation. This case is a representative application illustration; specific indices are customised per project requirements.

Conclusion

Orbital data centres push the boundary of compute into space, and place reliability demands on every basic component that the ground era never imagined.

JONSN micro magnetic gear pumps provide a trustworthy "heart" for space liquid cooling loops through their zero-leakage, high-precision, low-pulsation and long-life maintenance-free characteristics.

If your computing constellation, on-board edge node or space thermal control system is selecting a circulation pump, please contact the JONSN technical team for parameter matching and customised solutions tailored to your mission profile.

Frequently Asked Questions

Can gear pumps work normally in a microgravity environment?

Yes. JONSN micro gear pumps use a positive displacement structure that transports working fluid through gear volume change, and do not rely on gravity for drive. Magnetically coupled with no dynamic seals, there is also no cavitation-sensitive axial sealing interface, so flow remains stable and operation reliable under microgravity and high vacuum.

Which coolants are supported?

Compatible with deionised water, water-glycol, electronic fluorinated liquid (such as perfluorinated compounds) and ammonia — mainstream aerospace thermal control media. Pump cavity contact materials use stainless steel, PEEK and ceramic, offering good chemical compatibility and low outgassing characteristics.

How is radiation resistance?

The standard version has basic radiation tolerance. For long-duration low Earth orbit missions, radiation-hardened driver circuits and hardened electronics options are available to match the project's total ionizing dose (TID) budget.

Is the power consumption high?

At 100 mL/min and 10 bar the rated power consumption is ≤15 W, a friendly position within the satellite power budget, helping allocate more electrical power to the compute load.

What is the operating temperature range?

The pump body operating temperature covers -40 °C to +120 °C, adapting to the full mission profile including ground standby during the launch phase, thermal shock in the ascent phase and on-orbit hot-cold cycling.

How long is the service life, and can it be serviced on orbit?

The design maintenance-free operating life is ≥20,000 hours. Because servicing on site in space is impossible, the pump uses a structure with no dynamic seals and no consumable soft tubing — life equals the usable cycle of the system, matching the on-orbit mission.

Is customisation supported?

Yes. Drive voltage, fluid interface, contact materials and flow specifications can all be customised per project requirements, with small-batch space-grade screening and batch traceability supported.

What is the advantage over centrifugal or peristaltic pumps?

The core difference lies in the combination of "zero leakage + low pulsation + high precision + lightweight long life": centrifugal pumps carry dynamic seal leakage risk and perform poorly at small flow, while peristaltic pumps pulsate heavily and use consumable tubing. JONSN micro gear pumps offer better overall suitability in the non-serviceable space scenario.

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