Execute New Flight Plan

Warning Burn Time did not Match the Calculation

EROR 313: SYSTEM BURN TIME ERROR – ΔV EXCEED REMANNING FUEL

Station GNC Connect

Station GNC

Completion 1%
Altitude 3500 KM
Velocity 1400 m/s
RCS Thruster
Gyroscope
Startracker
Sun Position
Angular Velocity
Structure

Spacecraft Engine

Thrust 2%
Isp 0kN

Spacecraft Main Engine

PROGRAM NO
GSFC039104

FUEL
OXIDISER
FAULT CHECKER →

Lunar Gateway

Power

Power0%

Spacecraft power is nominal

SWU
PCDU
PC28
2000 m/s

ΔV to Burn

Spacecraft Engine

Burning
Connect
Burn Completion 1%

Remaning

Velocity to Burn

ΔV

2000 m/s

G
Gateway

L
Lunar

Targeting PE 3,000 AP 7,000

Aposelene 70000 KM