Arya Launch Vehicle

Space Station in a launch(Patent Pending 2025)

Key Features

The spacecraft consists of three primary zones, each engineered for specific functions:

1. Propulsion Zone

  • Located at one end, this section contains the rocket engine and critical support structures for propulsion during launch.

2. Central Compartmentalized Tank Zone

  • Dual Functionality: During launch, it stores liquid fuel (e.g., propane) and oxidizer (e.g., liquid oxygen).
  • Orbital Conversion: Once in orbit, the tanks are purged, pressurized, and transformed into living quarters or storage spaces, ensuring efficient utilization.

3. Payload Bay Zone

  • Equipped with:
    • Solar panels for sustainable energy generation
    • Batteries and life support systems for continuous operations
    • Communication modules for Earth and inter-station connectivity
    • Docking mechanisms for spacecraft attachments and expansions

Seamless Transition from Rocket Stage to Space Station

The spacecraft’s design enables a smooth and efficient transition process:

  1. Propulsion System Detachment: Using explosive bolts and electromechanical latches, the engine is safely jettisoned after its role is complete.
  2. Residual Propellant Venting: Remaining propellants are vented into space for safety.
  3. Tank Purging and Pressurization: Tanks are purged with inert nitrogen and pressurized to create a habitable or storage environment.
  4. System Activation: Life support systems, solar panels, and communication modules are activated for immediate operational readiness.

Why Choose This System?

  • Efficient Space Utilization: Dual-purpose functionality reduces the need for separate vehicles, saving time and resources.
  • Pre-Configured for Orbit: Designed for immediate use in space without additional modifications.
  • Sustainability in Space: Reduces debris and ensures optimal use of all spacecraft components.