The future of spaceflight
Developing the Vayu launch vehicle family. Targeting 150 kg to LEO (Expendable) by 2029.
Roadmap to Orbit
Our critical path to reusable orbital flight (2026 → 2030)
Foundation
- • HQ + engineering team
- • Test site construction
- • Engine test stand readiness
- • Pressure-fed engine development
Goal: Full-duration static fire.
Vayu-1 Sounding Test
- • 40 kN engine flight test
- • Avionics validation
- • Telemetry qualification
Suborbital data collection (Target).
Vayu-2 Orbital Att.
- • 250 kN engine ground test
- • Stage separation test
- • First orbital attempt
Target: First orbital launch attempt.
Commercial Payload
- • Payload integration
- • Mission assurance
- • 150 kg to LEO goal
Target: Commercial payload delivery (Expendable).
Recovery R&D
- • Propulsive landing tests
- • Grid fin aerodynamics
- • Low-altitude hops
R&D phase for reusable architecture.
Foundation
- • HQ + engineering team
- • Test site construction
- • Engine test stand readiness
- • Pressure-fed engine development
Goal: Full-duration static fire.
Vayu-1 Sounding Test
- • 40 kN engine flight test
- • Avionics validation
- • Telemetry qualification
Suborbital data collection (Target).
Vayu-2 Orbital Att.
- • 250 kN engine ground test
- • Stage separation test
- • First orbital attempt
Target: First orbital launch attempt.
Commercial Payload
- • Payload integration
- • Mission assurance
- • 150 kg to LEO goal
Target: Commercial payload delivery (Expendable).
Recovery R&D
- • Propulsive landing tests
- • Grid fin aerodynamics
- • Low-altitude hops
R&D phase for reusable architecture.
Launch & Test Schedule
Upcoming firing tests and launch windows.
| Date | Mission | Status |
|---|---|---|
| Q1 2027 | Vayu-1 Sounding Mission | Target |
| 2028 | Vayu-2 Orbital Test Flight | Target |
| 2029 | Commercial Payload Mission | Target |
| 2030+ | Recovery Tech Demo | R&D |
*All future dates are targets subject to testing qualification and regulatory confirmation.
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Advanced Propulsion
High-precision engine systems
Next-generation rocket engines designed for reliability, reusability, and maximum payload capacity.
Target Thrust
50,000 lbf Class
Design Reuse Goal
Target: 100+
Efficiency Goal
High Isp Arch.
Development Time
36 Months
*All milestones are targets based on current testing and program maturity and may change after qualification and regulatory approval.
Capabilities
Engineering metrics that matter
Vehicle Architecture
Recoverable
Design goal: Long-term reusability
Production Target
Rapid
Designing for 10-day vehicle integration
Cost Goal
-90%
Target reduction in $/kg vs legacy launchers
Launch Readiness
< 7 Days
Rapid integration target
Technology
Built from first principles
No shortcuts. No compromises. Just physics-first engineering at scale.
Vayu Engine
Primary propulsion system with 50,000 lbf class thrust rating
✓ Reusability Target
✓ High Efficiency Goal
✓ 100+ Cycle Life Goal
Precision Systems
Advanced guidance and autonomous flight control systems
✓ AI-driven
✓ Real-time adaptation
✓ High-reliability architecture
Recovery Platform
Autonomous landing and vertical recovery technology
✓ Vertical Landing R&D
✓ Rapid Turnaround Goal
✓ Simplified Ops
Engineering Philosophy
How we build
First Principles
Engineering from fundamental physics, not industry patterns.
Extreme Ownership
Every engineer builds. Every person is accountable for mission success.
Rapid Iteration
We move fast to test hypotheses. Rigorous testing validates every design choice.
Deep Work
No meetings culture. Deep focus on what actually matters for spaceflight.
Mission First
Humanity's multiplanetary future is worth every ounce of effort.
Join the mission
We're looking for exceptional engineers and operators who are obsessed with space and willing to spend years on hard problems that matter for humanity's future.
Making humanity multiplanetary. One mission at a time.