Design sheet · turbojet with reheat · sea-level static

Every figure is calculated in this page by one function, engineAt(), the same one the live engine uses. Air 288.15 K, 101.325 kPa. γ 1.4, R 287 J/(kg·K), LHV 43.0 MJ/kg. Stations 2–7 are total values.
AUTORUN 01 · T+00:00.0
288 Kgas temperature1,950 K
↑ ↓ throttle · R reheat · C cutaway · B chicken gun
Space autopilot · M mute · drag to orbit · wheel to zoom
Click for sound
MAX DRY · the engine is already running
TEST CELL: the neighbours have been told.
STATIC THRUST
0.0
kN
T–s DIAGRAM · s from station 2