Isar Spectrum Orbital Launch Simulator

Flight Mission Profile SPECTRUM V1

LAUNCH VEHICLE PRESET

PAYLOAD MASS 700 kg

PITCH-KICK ANGLE (α) 3.8°

GRAVITY TURN ALTITUDE 2,500 m

TARGET INSERTION PERIGEE 500 km

Staging Parameters

Stage 1: 9x Aquila Propane/LOX Cluster

Stage 2: 1x Aquila Vacuum Engine

Total Propellant: 48,000 kg

Stage 1 Burn: 142 s | S2: 280 s

PRE-FLIGHT READY

Configure launch parameters and initiate the burn to evaluate Norwegian polar trajectory.

NORWEGIAN SEA FLIGHT CORRIDOR

INCLINATION: 97.8° (SSO)

T-00:00:00 (PAD IDLE)

Ascent Stage Telemetry Log 0 checkpoints

MET (s)	Altitude (km)	Downrange (km)	Velocity (m/s)	Mach	Dyn-Q (kPa)	Event
Awaiting ignition sequence...

Flight Dynamics T+00:00

ALTITUDE

0.0km

TOTAL VELOCITY

0m/s

DOWNRANGE

0.0km

MACH SPEED

0.00M

APOGEE (Ha)

0km

PERIGEE (Hp)

-6371km

MAX-Q DYNAMIC PRESSURE 0.0 kPa (0%)

STAGE 1 PROPELLANT (Aquila Cluster) 100%

STAGE 2 PROPELLANT (Aquila Vac) 100%

TOTAL ACCUMULATED ΔV 0 / 9,250 m/s

Polar SSO Launch Guidance

Launching northward from Norway's Andøya Spaceport bypasses European landmasses directly over the Norwegian and Barents Seas into Sun-Synchronous Orbit.

Target Orbital Velocity: 7,612 m/s

Gravity Loss Allowance: ~1,150 m/s

Atmospheric Drag Loss: ~140 m/s