VectraSpace // Mission Control
⬆ Trajectory Simulator
Suborbital RK4 — WGS84 Gravity — Exp. Atmosphere
Rocket Properties
Mass (kg)
total wet mass
Cd
drag coefficient
Ref. Area (m²)
cross-section — πr² for cylindrical body
Motor
A
B
C
D
E
F
G
H
I
J
K
Total Impulse (N·s)
Burn Time (s)
Launch Geometry
Angle from Vertical (°)
0 = straight up
Azimuth (°)
clockwise from N
Launch Site
Latitude (°)
Longitude (°)
Site Altitude (m ASL)
▶ Run Simulation
✓ Simulation Complete
Apogee
—
m
Max Velocity
—
m/s
Flight Time
—
s
Surface Range
—
km
Landing Zone
—
↓ Export CSV
Last Trajectory
Apogee:
—
T-flight:
—
V-max:
—
Computing Trajectory