Reusable Launch Systems

Engineering the Future of Space Access

Cosmo Crawler is developing next-generation reusable rocket technology with hybrid landing systems — reducing launch cost, operational risk, and barriers to orbit.

100% Reusable Vision
3D Printed Engines
Hybrid Landing Tech
Cosmo Crawler reusable rocket concept

About Cosmo Crawler

Building India's pathway to fully reusable launch vehicles through advanced propulsion and landing innovation.

From Prototype to Orbit

Cosmo Crawler is on a mission to develop a fully reusable launch vehicle. Our journey began with designing and cold-testing a small liquid rocket engine — powered by next-generation propellants for cleaner, more efficient combustion.

  • Electric pump-fed liquid rocket propulsion
  • Aerospace-grade 3D-printed engine components
  • Hybrid landing systems for safer recovery
  • Cost-effective access to space for emerging markets
Rocket propulsion engineering
Mission Advance space exploration through reusable innovation

Our Technology

Three pillars driving the next era of affordable, reliable space transportation.

Reusable Rockets

Designing launch systems built for multiple flights — dramatically lowering per-kilogram launch costs and enabling sustainable space operations.

Hybrid Landing

Our hybrid landing approach combines proven recovery methods with novel control systems to reduce landing risk and improve vehicle turnaround time.

Next-Gen Propulsion

Advanced liquid rocket engines using next-generation propellants, electric pump feed systems, and additive manufacturing for rapid iteration.

Prototype

Prototype 1: Reaction Control Engine

Our first engine prototype is fully 3D-printed in a super aluminum-silicon alloy (Al-Si) — an aerospace-grade material. Assembled with spray pump motors for initial testing, it underwent cold testing with ignition to characterize dynamic combustion properties.

The engine operates on next-generation rocket propellants and is driven by an electric pump feed system — validating our core propulsion architecture before scaling to full thrust.

Watch the engine fire test (2 angles)

Al-Si Alloy Electric Pump Feed Cold-Fire Tested 3D Printed

Engine Fire Test

Real cold-fire ignition footage of our reaction control engine — captured from two camera angles during live testing.

Camera Angle 1

Side View — Ignition & Burn

Side-angle capture showing engine ignition, flame stability, and exhaust plume during the cold-fire test sequence.

Camera Angle 2

Alternate View — Full Test Run

Second camera perspective documenting the complete firing event, validating combustion performance from another vantage point.

CAIMAN 2000

Micro-Category Liquid Rocket Engine

The CAIMAN 2000 is a fully 3D-printed liquid rocket engine in the micro-thrust class. It features continuous restart capability without thrust degradation — a critical requirement for precision maneuvering and landing operations.

1,000 kgf Thrust at 60 bar chamber pressure
2,200+ kgf Maximum thrust at full power

Our Team

A multidisciplinary team of engineers, scientists, and technicians delivering cutting-edge solutions for the space industry.

Yoga Raj

Yoga Raj

Founder
Dr. S. Ekambaram

Dr. S. Ekambaram

Advisor — Physical Chemistry
K. Reivanth

K. Reivanth

Advisor — Materials Science
Bharath Karthick

Bharath Karthick

Research Assistant
Naveen Kumar

Naveen Kumar

Engineering Team
Ramanan

Ramanan

Project Associate

Funded By

Supported by organizations that believe in advancing aerospace innovation.

Supported By

Partners and institutions empowering our research and development.

Contact Us

Interested in partnerships, investment, or collaboration? We'd love to hear from you.

Location

21, Karunanithi 2nd Cross Street, West Mambalam, Saidapet, Chennai 600033, India

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