About

Guerin Technologies is an aerospace engineering and technology development company dedicated to advancing the future of space systems through innovative mechanical engineering.

Our focus is on developing mission-critical aerospace hardware, precision mechanisms, actuation systems, deployable structures, and advanced engineering solutions that enable reliable operation in challenging environments.

We believe that breakthrough aerospace technologies are built through rigorous engineering, continuous research, and a commitment to reliability.

Systems

Specialized mechanism systems house — release devices, dampers, deployable booms, spring hinges, and motorless architectures for launch shock, vacuum, and long-life orbit.

Composite deployables

Carbon-composite booms, rollable structures, and spring-hinge architectures sized for stowage volume and orbital stiffness targets.

Release & separation

Low-shock separation bolts and synchronized release rings tested for pyro-shock and cleanliness envelopes.

Dampers & deployment control

Eddy-current and viscous damping for hinge-rate control — zero leakage paths, predictable deployment kinematics.

Full-stack qualification

End-to-end qualification — design through AIT and space test for deployables, releases, dampers, and deployment control.

Products

Mechanisms in active development — select a subsystem for engineering specifications, qualification envelopes, and integration detail. Each product line is scoped for flight-critical release, damping, and deployment applications across LEO, GEO, and deep-space mission profiles.

Photorealistic 3D render of space-grade titanium separation bolt actuator with Kapton wrapping

Fracteon

Low-shock, clean mechanical separation mechanism designed for highly synchronized spacecraft release ring applications.

Low-shock, clean mechanical separation mechanism designed for highly synchronized spacecraft release ring applications. Engineered for minimal pyro-shock transfer, high cleanliness, and repeatable actuation across qualification and flight units.

Click the image for more details

Photorealistic 3D render of aerospace eddy current damper rotor disk and magnet housings

ECD

Magnetic hysteresis non-contact rotational damper offering zero outgassing, zero leakage, and near-infinite life.

Magnetic hysteresis non-contact rotational damper offering zero outgassing, zero leakage, and near-infinite life. Velocity-proportional torque for controlled deployment without fluid paths, seals, or maintenance-prone wear surfaces in vacuum.

Click the image for more details

Photorealistic 3D render of spring-driven satellite solar array deployment hinge

Deployable Hinge

Spring-driven satellite deployment hinge offering positive latching force, zero backlash, and position triggers.

Spring-driven satellite deployment hinge offering positive latching force, zero backlash, and position triggers. Built for solar arrays, radiators, and boom deployments requiring deterministic kinematics and hard-stop repeatability after launch loads.

Click the image for more details

Photorealistic 3D render of spacecraft rotary viscous damper with double seal containment barriers

RVD

Precision fluid-damping mechanism engineered with dual-barrier seals and high-viscosity silicone fluid.

Precision fluid-damping mechanism engineered with dual-barrier seals and high-viscosity silicone fluid. Tuned for hinge-rate control on deployable structures where predictable deployment speed and containment integrity are mandatory for mission success.

Click the image for more details

Patents

Two mechanism families — SURA and SUSA — for rollable, motorless deployables, sharing proven qualification heritage.

Self-unwinding reflector array antenna deployed on a spacecraft

SURA

Self-Unwinding Reflector Array

Indian patent grantedPCT filed

Motorless antenna — compact roll stow, composite architecture tuned for mass, volume, and deployment reliability.

Rollable solar array wing using motorless deployment mechanism

SUSA

Self-Unwinding Solar Array

Mechanism patent pendingSURA heritage

Solar wing on the same motorless physics as SURA — high compactness and faster qualification via shared mechanism IP.

Collaboration

ISRO antenna programme · AI Craft deployable systems co-development.

Incubated at IISc ART Park · IIMA Ventures · Social Alpha.

IIMA Ventures

IISc

AI Craft

Social Alpha

ISRO

  • IIMA Ventures

    IIM Ahmedabad incubation · DST Centre of Excellence

  • IISc

    Incubated at IISc ART Park

  • AI Craft

    Co-developing deployable systems

  • Social Alpha

    Incubation · Tata Trusts FISE TBI

  • ISRO

    Active antenna programme collaboration

Founders

Leadership across strategy, partnerships, and mechanisms engineering — from research lineage through flight hardware delivery.

Suhas Bannur

Founder & CEO

Directs corporate strategy, global partnerships, production QA, and compliance architecture. Drives alignment with global space agencies and satellite builders.

Credentials: IIM Bangalore & IISc Bangalore Research Alumnus
Click for biography

Dr. Abhilash

Founder & CTO

Directs mathematical modeling, finite element analysis (FEA), mechanical engineering, and technical operations.

Credentials: IIT Madras PhD, IISc Bangalore Alumnus
Click for biography
T-MINUS 3... IGNITION SEQUENCE START