LAUNCHER Simulator
Stage 1
Propellant 1
:
LOX-RP1
Solid
Propellant mass
(kg):
Propellant type 1:
Isp1 (s):
Structural index 1 :
Total mass 1 (kg):
Propellant mass 1 (kg):
Structural mass 1 (kg) :
Stage 2
Propellant 2
:
LOX-RP1
LOX/LH2
-
Propellant mass
(kg):
Propellant type 2:
Isp2 (s):
Structural index 2 :
Total mass 2 (kg):
Propellant mass 2 (kg):
Structural mass 2 (kg) :
Stage 3
Propellant 3
:
LOX-RP1
LOX/LH2
-
Propellant mass
(kg):
Propellant type 3:
Isp3 (s):
Structural index 3 :
Total mass 3 (kg):
Propellant mass 3 (kg):
Structural mass 3 (kg) :
Payload & Fairing
Payload mass
(kg) :
Fairing mass
(kg) :
Total mass
Total mass(kg) :
Security message :
Launchpad
Launchpad
:
Kourou
Cap Canaveral
Baikonur
Vandenberg
Latitude
(deg):
Azimuth
(deg):
Injection
Altitude
(km):
Slope
(deg):
Mission
Mission
:
-
Mission 1
Mission 2
Mission 3
Mission 4
Launcher
ΔV
(m/s) :
Losses
(m/s):
Earth velocity gain
(m/s) :
ΔV1
(m/s) :
ΔV2
(m/s) :
ΔV3
(m/s) :
Velocity at injection
(m/s) :
Total mass
(kg) :
Orbit
Semi-major axis
(km):
Eccentricity
:
Inclination
(deg) :
Perigee altitude
(km):
Apogee altitude
(km) :
Period
(min) :
Telemetry
Perigee :
Apogee :
Inclination :
Telemetry message :