šŸš€ Space Technology Simulator

Design rockets, plan missions, and explore the cosmos with realistic space physics

šŸš€ Rocket Design Laboratory

šŸ›°ļø
Command Module
Crew: 3-7
⛽
Fuel Tank
Capacity: 500t
šŸ”„
Rocket Engine
Thrust: 2000kN
šŸš€
Solid Booster
Extra Thrust
šŸ›”ļø
Payload Fairing
Protection
🦵
Landing Legs
Reusable

šŸŒ Orbital Mechanics Simulator

Orbital Parameters

Altitude: 400 km
Inclination: 51.6°
Eccentricity: 0.00

šŸ”“ Mars Mission Planner

Mission Parameters

Launch Window:
Mission Duration: 600 days
Crew Size: 4 people

šŸ›°ļø Satellite Deployment

Satellite Configuration

Satellite Type:
Deployment Altitude: 550 km

šŸŽ›ļø Mission Control

šŸ“” Telemetry Data

Velocity: 7.66 km/s
Altitude: 408 km
Fuel Remaining: 78%
Mission Time: T+ 00:45:32
Distance to Target: 2,847 km

ā° Launch Sequence

T-10 Pre-launch checks
T-5 Engine ignition
T-0 Liftoff
T+30 Max Q
T+120 Booster separation
T+480 Orbit insertion

🚨 System Status

Main Engines: NOMINAL
Life Support: NOMINAL
Communications: INTERMITTENT
Navigation: NOMINAL
Power Systems: NOMINAL

šŸŽÆ Mission Objectives

āœ… Launch successful

ā³ Reach target orbit

ā³ Deploy payload

ā³ Establish communication

ā³ Mission duration: 6 months

šŸ“š Space Facts

• ISS orbits Earth every 90 minutes

• Escape velocity from Earth: 11.2 km/s

• Mars is 54.6M km away at closest

• Voyager 1 is 24B km from Earth