Test Cell 07 — Single-Spool Turbojet, Reheat

OPEN-AIR STAND · SEA LEVEL, STANDING STILL · AMBIENT 288.15 K / 101.325 kPa
ONE PERFECT GAS γ=1.4, R=287 J/(kg·K) · FUEL MASS NOT ADDED TO THE GAS STREAM · ALL NUMBERS CALCULATED IN THIS PAGE

Particle colour — local gas temperature

288 K700110015001950 K

Design sheetcomputed from the engine data, not typed in

Station / quantity	IDLE	MAX DRY	MAX REHEAT
Gas generator
T03 K
p03 kPa
T05 K
p05 kPa
T07 K
p07 kPa
Propelling nozzle & performance
Exit Mach M9
Jet speed V9 m/s
Nozzle area A8 m²
Static thrust kN
Fuel burned kg/s
Fuel / thrust g/kN·s
Compressor shaft MW

Temperature – entropylive

Δs from station 2, J/(kg·K)dashed = design MAX DRYT, K

Event logrun 1

Controlsmouse drag = orbit · wheel = zoom

↑↓ throttle

R reheat

C cutaway

B chicken gun

Space autopilot

M mute

T+00:00.0 TEST CELL ONLINE — MAX DRY AUTO

Thrust

0.0kN

static, sea level

Spool speed

100.0%

EGT · T05

Fuel burned

0.00kg/s

Nozzle area A8

0.000m²

Throttle 100%