TAILWIND

Non-toxic chemical propulsion for ESPA-class LEO satellites.

Technical  Specifications

Total impulse
22,500 Ns
Thrust range
1,000 to 5,600 mN
Deep individual throttle control of all 4 thrusters
Power, firing
150 to 614 W 
Scales linearly with commanded thrust level
Propellants
Nitrous oxide (N2O) & Ethane (C2H6)
Environment
>20 krad TID & 5 to 30 °C 
Mass
Wet: 29.0 kg / Dry: 18.4 kg
Envelope
550 × 360 × 275 mm

Chemical when you need agility

Orbit change

Commissioning after launch, or repositioning for the mission.

Electric
Months
Chemical
Days

Collision avoidance

Debris or a threat, often with short warning.

Electric
Days
Chemical
Minutes

Proximity operations

Moving close to another satellite to inspect, repair or refuel.

Electric
Not possible
Chemical
Agile, precise
TAILWIND propulsion system, close-up

TAILWIND

  • 1,000× higher thrustCompared to electric systems used today
  • Green propellantsNon-toxic, self-pressurizing and cheap
  • Reliable ignitionWith our patent pending fluid system
  • 50 systems per yearProduction capacity in new facilities
  • Built to ship from stockTarget: 1-month lead time for standard units, vs. typical 9–18 months

Simple by design

Two tanks. Four thrusters. Dual redundant power and data interface.

No pressurant, no pumps, no catalyst.

TAILWIND, top viewTAILWIND, underside view

Documentation, modernised

The full TAILWIND user's guide, online and searchable. One reference from selection to operations.

Request access to the user's guide

Flexible thrust, flexible power

Commanded thrust

3,000 mN

Firing power

352 W

1,000 mN5,600 mN

Thruster 1

750 mN

Thruster 2

750 mN

Thruster 3

750 mN

Thruster 4

750 mN

High thrust on a small-sat power budget. Pick any level from 1 to 5.6 N, command a single number, and TAILWIND balances it across all four thrusters automatically.

Features that makes it work

>20 kRad

TID radiation tolerance for 5 years in LEO.

PhaseGuard

Increase ignition reliability with our patent-pending fluid management system.

SpinLock

Keeps thrust autonomously aligned through the centre of mass.

TAILWIND hardware

Tailored for rideshare

Front view
TAILWIND on rideshare plate, front view
Bottom view
TAILWIND on rideshare plate, bottom view
Isometric view
TAILWIND on rideshare plate, isometric view

We designed TAILWIND around rideshare from the very first sketch, shaping it to fit the space that is already there. The thrusters sit inside the 24" separation ring, using just 91 mm of the 177.8 mm intrusion allowance on a SpaceX Rideshare Full / XL Plate, so TAILWIND fits a wide range of platforms without redesigning the satellite.

Made for serial production

TAILWIND thruster held in a gloved hand, more thrusters behind

Every part of TAILWIND is engineered for manufacturability from day one, so we can build systems in series, not one at a time. Our patent-pending thruster manufacturing process gives regenerative cooling without any additive manufacturing. It is the first time this has been done for a thruster of this size anywhere in the world.

Next available delivery: May 2027 (Q2)

Order a TAILWIND propulsion system

Unit price

€400,000

Included

  • Full standard TAILWIND system
  • Documentation
  • Propellant
  • Filling
  • Support

Quantity

Total €400,000
1

Configuration

Standard configuration
Modified configuration
Book a call
  1. 1Place your order
  2. 2NDA sent for signature within 2 business days
  3. 3Order confirmation within 2 business days of the signed NDA

Your order is confirmed once checks are complete and both parties have signed. See our Order Terms.

Included and optional services

INCLUDED IN THE UNIT PRICE

  • PropellantTAILWIND is delivered with propellant included in the price.
  • Propellant fillingWe fill TAILWIND once for your satellite's environmental test campaign and once at the launch site, with our own equipment. Travel and days on site included.
  • 20 hours of engineering supportFrom contract signature until delivery.
  • 10 hours of in-orbit supportRemote support during the first month after launch.
  • Full documentation packageStructural and load models, mass data, plume analysis, command list and acceptance test results for your unit.

Optional

  • Electrical and software modelsDevelop and test your interface to TAILWIND before the flight unit arrives.
  • Product modificationsLarger tanks, eight thrusters or thrusters placed differently.
  • Mission planning and analysesOrbit simulations and extra analyses, such as exhaust plume.
  • Extra fillingsAdditional fillings or emptying, for example if your launch is delayed.
  • Extended support and warrantyAdditional engineering hours, monthly support after launch and extended warranty.
Discuss a custom configuration

FAQ

Let's talk propulsion.
We're ready when you are.

TAILWIND: non-toxic bipropellant propulsion for ESPA-class LEO satellites

TAILWIND is a non-toxic chemical propulsion system for ESPA-class satellites in low Earth orbit. It is a self-pressurizing bipropellant system running on nitrous oxide (N₂O) and ethane (C₂H₆), with no pressurant tank, no pumps and no catalyst bed. Four thrusters deliver 1 to 5.6 N of thrust and 22,500 Ns of total impulse at a specific impulse of 206 to 242 s. Power draw scales linearly with thrust, from 150 to 614 W. There is no catalyst to preheat, so the system goes from idle to full thrust in under 30 seconds. PhaseGuard (patent pending) vaporizes liquid in the feed lines so only gas reaches the thrusters, which removes the leading cause of ignition failure in self-pressurized systems. SpinLock throttles each thruster individually using an internal IMU and holds the net thrust vector through the centre of mass, with no ADCS input needed during the burn.

TAILWIND weighs 29.0 kg wet and 18.4 kg dry. Its envelope is 550 × 360 × 184 mm above the base plate, with an overall height of 275 mm. The thrusters sit below the spacecraft bottom plate, inside the separation ring, and are compatible with the SpaceX Rideshare Full Plate and XL Plate with Intrusion and the Exolaunch CarboNIX 24″ ring. A single interface panel carries dual-redundant power feeds and CAN buses running CubeSat Space Protocol. Almost no heat soaks into the spacecraft, and the exhaust of water, carbon dioxide and nitrogen leaves near-zero residue on optics and solar arrays. Design life is 5 years, electronics are radiation-qualified above 20 krad TID, and the system is ITAR-free. Total impulse scales with tank length, and the thruster count can be increased to eight for single-failure tolerance. Qualification follows ECSS with a QM/FM philosophy. TAILWIND is built in Copenhagen, Denmark, with flight units available for delivery from May 2027 (Q2).