Building Tomorrow's Space Technology

Revolutionizing Space
Exploration

Trajectory Inc. is revolutionizing space exploration through cutting-edge satellites, advanced rocket engines, intelligent humanoid robots, and our own locally-manufactured rocket fuels powered by our hydrogen production facility. Our flagship Thruster propulsion system powers the innovative Trajectile rocket for tomorrow's space missions.

Satellites
Advanced Communication
Thruster
Rocket Engine
Robots
Humanoid AI
H₂ Plant
Fuel Production
Local Fuel Manufacturing

Liquid Hydrogen Fuel Systems

Our locally-manufactured rocket fuels, Liquid Hydrogen (LOH) and Liquid Oxygen (LOX), are produced from abundant local resources, ensuring reliable fuel supply and reducing launch costs while supporting Uganda's emerging space industry.

LOH & LOX Production

Locally-Sourced Rocket Fuels

LOH
Liquid Hydrogen
-253°C Storage
LOX
Liquid Oxygen
-183°C Storage
6:1
O/F Ratio
Optimal Mix
450s
ISP Rating
High Performance

Local Production Advantages

Water Electrolysis from Lake Victoria

Abundant water resources provide sustainable hydrogen production

Atmospheric Oxygen Extraction

Air separation units capture and purify oxygen locally

Hydroelectric Power Integration

Clean energy from Uganda's hydro infrastructure powers production

Strategic Location Benefits

Equatorial location ideal for efficient satellite launches

Production Facility

Production Process

H₂O Electrolysis 2,400 kg/day
Air Separation 14,400 kg/day
Liquefaction 99.9% Purity

Storage Infrastructure

50,000L
LOH Storage
300,000L
LOX Storage

Quality Assurance

Purity Level 99.95%
Contamination < 50 ppm
Temperature Control ±0.1°C

Economic & Environmental Impact

Cost Reduction

45% lower fuel costs through local production vs. imported alternatives

$2.8M
Annual Savings

Job Creation

Direct employment in fuel production, storage, and quality control

150+
Local Jobs

Clean Energy

100% renewable energy powered production with zero carbon emissions

Zero
CO₂ Emissions

Supply Chain Independence

Local Resources
  • Lake Victoria water supply
  • Atmospheric oxygen extraction
  • Hydroelectric power grid
  • Local technical expertise
Strategic Advantages
  • Reduced logistics complexity
  • Elimination of import dependencies
  • Real-time quality control
  • Rapid launch turnaround times
Advanced Propulsion System

The Thruster Engine

Our revolutionary Thruster engine represents the pinnacle of rocket propulsion technology, featuring advanced full-flow staged combustion and unmatched performance capabilities for the next generation of space missions.

Thruster Engine

Advanced Rocket Propulsion

2.5M
lbf Thrust
Sea Level
450s
Specific Impulse
Vacuum
CH₄/LOX
Propellant
Methane/Oxygen
100+
Reuse Cycles
Operational Life

Advanced Features

Full-Flow Staged Combustion Cycle

Maximum efficiency through complete propellant combustion

Regenerative Cooling System

Fuel-cooled nozzle and combustion chamber design

Variable Thrust Control

Deep throttling capability from 40% to 100% thrust

Rapid Reusability Design

Minimal refurbishment between flights

Thruster Engine

Performance Metrics

Chamber Pressure 300 bar
Combustion Efficiency 98.7%
Mass Flow Rate 685 kg/s

Engine Technology Breakdown

Combustion

Advanced injector design ensures optimal fuel-oxidizer mixing for complete combustion efficiency.

Cooling

Regenerative cooling channels machined into the nozzle provide superior thermal management.

Control

Precision thrust vectoring and throttling capabilities enable precise mission control.

Heavy-Lift Launch Vehicle

The Trajectile Rocket

Powered by our Thruster engine, the Trajectile rocket is designed for versatile space missions, from satellite deployment to deep space exploration with unprecedented reliability and cost-effectiveness.

Trajectile Rocket

Mission Capabilities

LEO
Low Earth Orbit
GTO
Geostationary Transfer
TLI
Trans-Lunar Injection
IPT
Interplanetary

Trajectile Rocket

Heavy-Lift Launch Vehicle

70m
Height
Total Vehicle
3.7m
Diameter
Core Stage
1,420
Tonnes Mass
Fully Fueled
22.8
Tonnes to LEO
Payload Capacity

Stage Configuration

First Stage
9 Engines
Engines: 9 × Thruster
Thrust: 22.5M lbf
Fuel: 1,200,000 kg
Burn Time: 162 seconds
Second Stage
1 Engine
Engines: 1 × Thruster Vac
Thrust: 2.8M lbf
Fuel: 135,000 kg
Burn Time: 397 seconds

Launch Performance

$62M
Launch Cost
95%
Recovery Rate
3.5
Days Turnaround
50+
Mission Types

Payload Configurations

Satellite Deployment

Multiple satellite deployment for constellation missions

Up to 120 satellites

Space Stations

Large modules and cargo for space station operations

22.8T capability

Deep Space

Interplanetary probes and exploration missions

8.3T to Mars
Development Progress

Development Timeline

Track our progress as we develop the Thruster engine and Trajectile rocket from concept to flight-ready systems.

Phase 1: Design & Research

Completed

Q1 2022 - Q4 2023

  • Thruster engine conceptual design
  • Trajectile vehicle architecture
  • Advanced materials research

Phase 2: Prototype Development

Completed

Q1 2024 - Q3 2024

  • First Thruster engine prototype
  • Static fire testing campaign
  • Trajectile tank development

Phase 3: Integration & Testing

In Progress

Q4 2024 - Q2 2025

  • Full-scale engine testing
  • Trajectile stage integration
  • Ground systems validation

Phase 4: Flight Testing

Planned

Q3 2025 - Q1 2026

  • First Trajectile test flight
  • Orbital demonstration mission
  • Commercial certification

Development Progress

Overall Completion

Design & Research 100%
Prototype Development 100%
Integration & Testing 75%

Key Achievements

127
Engine Tests
450s
ISP Achieved
85
Design Reviews
99.8%
Test Success