SPECIFICATIONS

LIFTOF MASS

150 000 KG

LIFTOFF THRUT

2.5 MN

MAX PAYLOAD

25 000 KG

MAX ALTITUDE

200 KM

PAYLOAD TO GTO

1 500 KG

FIRST STAGE ENGINE

M-250 (×1)

FIRST STAGE ENGINE ARCHUTECTURE

GAZ GENERATOR

FIRST STAGE ENGINE CAPACITY

2.5 MN / 315 s (sl)

HEIGHT

25 m

DELAY BETWEEN TWO FLIGHT

48 H

REUSABILITY

FULLY

LAUNCH COST

2 000 000 $

FIRST LAUNCH DATE

2027 - 2028

OVERVIEW

PAYLOAD

GRID FINS

battery / COPV

M-250 (×1)*

FAIRING

RCS THRUSTER

FIRST STAGE TANK (LCH4/LOX)

DEPLOYABLE HEAT SHIELD

FAIRING DIMENSION

5 m

5.5 m

1.25 m

1.5 m

1.25 m

1 m

1.2 m

1 m

3.5 m

FLIGHT TIMELINE

(1) launch, (2) ascent, (3) hot-staging, (3.1) heat shield closure / booster descent, (3.2) parachute deployment (4) fairing separation, (4.1) fairing re-entry, (4.2) parachutes deployment, (5) second stage thrust, (6) payload deployment.

DIFFERENT CONFIGURATIONS

Large fairing

small fairing

Suborbital plane

BOOK A FLIGHT

T-5S