Who:

Vortex Thrusters

Fluid:
working consumption: NONE
Thrust:
reversal: Available
ENERGY:
specific consumption: < 100 W/G
Control:
over primary angles: Available
Thrust, N:
0.2 - 1
MASS:
5 kg
Goal:
Possible Practical Applications

Description of the design and technical specification

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1. Mounting frame

2. Commutative
board

3. Control
board

4.Power frame with
thrusters and
fluid reservoir

5. Thermal reflector

6. Built-in radiator

Parametr: Value:
Working fluid consumption NONE
Thrust reversal Available
Control over primary angles 3 flight axes: pitch, yaw, roll
Specific energy consumption, W/G < 100 W/G
Thrust, N 0.2 - 1
MASS 5 kg

Example of the General View of a Spacecraft with a Vortex Thruster

(Thermal Protection System Not Shown)

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1. Capability to position the propulsion system directly at the spacecraft’s center of mass.

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Antena

Ka-band

Battery Unit

Payload

(docking and capture control system)

2. Modularity of Configurations.

Variability of Payload Configurations

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Optical surface sensing

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Interorbital tug

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Radar imaging

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Delivery variants

VARIANT A:

Clustered configuration in the payload compartment

VARIANT B:

Light-class launch vehicle

Propulsion Systems for Fuel-Free Manned and Automated Vehicles of Various Practical Applications

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Advantages:
  • 1. Simplicity.
  • 2. Maintainability.
  • 3.Reduction of parasitic mass.
  • 4.Capability for multiple orbital changes.
  • 5.Virtually unlimited operational lifespan.
Welmont CEO & Founder
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Space Stations

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Manned Spacecraft

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Automated Spacecraft

Interorbital Tugs and Lunar Shuttles

  • 1.Boosting to higher orbits or deorbiting.
  • 2.Fuel delivery.
  • 3.Supplying lunar space stations.
  • 4.Spacecraft acceleration.

Exploration of Deep Space

Flight duration at 1N thrust

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Servicing of Multi-Satellite Constellations

  • Satellite inspection.
  • Replacement of malfunctioning units.
  • Positioning adjustment.
  • Transport to repair stations.
  • Forced deorbiting.

Exploration of Deep Space and its Individual Objects

Kuiper Belt, Oort Cloud, outer planets of the Solar System

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Long-Distance

Vehicles for Long-Distance Missions
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Outer planets

Saturn: 8–11 AU
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Kuiper Belt

Kuiper Belt: 50 AU, Oort Cloud: 100 AU
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Fully Autonomous Station-Based Constellations

Key Tasks of the Station-Based Constellation

  • Station inspection.
  • Transport of satellites to repair stations.
  • Deployment of satellites to target orbits.
  • Replacement of satellites in designated orbits.

Transport of Space Objects

  • 1. Space debris cleanup.
  • 2. Transport of small space objects (mineral extraction).
  • 3. Deorbiting of potentially hazardous space objects from Earth’s orbit.

Inspector Satellites for Monitoring Artificial Space Objects

FUNCTIONS:

  • Orbital parameter verification.
  • External inspection.
  • Assessment of purpose, capabilities, and design features.
  • Identification of data exchange methods with Earth.

Takeoff/Landing and Flight to Small Solar System Objects (Asteroids)

FUNCTIONS:

  • Determination of chemical composition and potential value.
  • Sample collection.
  • Surface characterization and imaging.
  • Landing for subsequent joint flight operations.

Propulsion of Vehicles in Environments Where Direct Contact Between Thrusters and the Surroundings is Undesirable or Impossible

Propulsion of deep-sea vehicles on Earth.

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Vityaz, 2020.

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Trieste, 1960.

Propulsion of deep-sea vehicles for exploring extraterrestrial oceans (in space).

Exploration of the ocean on Jupiter’s moon (Europa).

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Market Capacity Assessment

Number of satellites in multi-satellite constellations. Evolution of the number of objects in geocentric orbit by object class.

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Constellation: Quantity, units:
StarLink 1- ~5 000; 2- ~30 000
OneWeb ~ 900
Сфера ~ 170

Key Conclusions

The implementation of vortex thrusters in routine practice enables:

  • Significant expansion of capabilities and increased versatility for current and future space missions.
  • Simplification of spacecraft design, reduction of parasitic mass, and increased flight duration and speed.

Reduction in the cost of space services through:

  • Decreased frequency of launch vehicle launches.
  • Extended operational lifespan of spacecraft.
  • Capability for in-space repairs.
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Contact Us:

Tel. (WhatsApp) +382 69-292545
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- Welmont