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SPECIFICATIONS
LIFTOF MASS
700 000 KG
LIFTOFF THRUT
10 MN
PAYLOAD TO LEO
30 000 KG
PAYLOAD TO SSO
19 500 KG
PAYLOAD TO GTO
10 000 KG
FIRST STAGE ENGINE
M-250 (×4)
FIRST STAGE ENGINE ARCHUTECTURE
GAZ GENERATOR
FIRST STAGE ENGINE CAPACITY
2.5 MN / 315 s (sl)
SECOND STAGE ENGINE
M-250V (×1)
SECOND STAGE ENGINE ARCHITECTURE
GAZ GENERATOR
SECOND STAGE ENGINE CAPACITY
2.5 MN / 340s (vac)
HEIGHT
61 m
DELAY BETWEEN TWO FLIGHT
48 H
REUSABILITY
FIRST STAGE / FAIRING
LAUNCH COST
25 000 000 $
RELEASE DATE
2027 - 2028
OVERVIEW
PAYLOAD
SECOND STAGE TANK (LCH4/LOX)
HOT STAGE RING
GRID FINS
battery / COPV

M-250 (×4)
FAIRING
M-250 ENGINE (×1)*
RCS THRUSTER
FIRST STAGE TANK (LCH4/LOX)
DEPLOYABLE HEAT SHIELD
FAIRING DIMENSIONS

8 m
8.5 m
2 m
2.5 m
2 m
1.5 m
2 m
1.5 m
5.5 m
5.5 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
Shuttle
T-30
T-13
T-70

SPECIFICATIONS :
LIFTOF MASS
1 900 000 KG
LIFTOFF THRUT
30 MN
PAYLOAD TO LEO
70 000 KG
PAYLOAD TO SSO
45 000 KG
PAYLOAD TO GTO
24 300 KG
FIRST STAGE ENGINE
M-250 (×12)
FIRST STAGE ENGINE ARCHUTECTURE
GAZ GENERATOR
FIRST STAGE ENGINE CAPACITY
2.5 MN / 310 s (sl)
SECOND STAGE ENGINE
M-250 (×1)
SECOND STAGE ENGINE ARCHITECTURE
GAZ GENERATOR
SECOND STAGE ENGINE CAPACITY
2.5 MN / 340s (vac)
HEIGHT
67 m
DELAY BETWEEN TWO FLIGHT
72 H
REUSABILITY
FIRSTS STAGES / FAIRING
LAUNCH COST
55 000 000 $
RELEASE DATE
OVERVIEW

PAYLOAD
SECOND STAGE TANK (LCH4/LOX)
HOT STAGE RING
GRID FINS
COPV
M-250 (×12)
LEFT BOOSTER
FAIRING
M-250 engine (×1)*
RCS THRUSTER
RIGHT BOOSTER
FIRST STAGE TANK (LCH4/LOX)
DEPLOYABLE HEAT SHEILD
FAIRING DIMENSIONS

8 m
8.5 m
2 m
2.5 m
2 m
1.5 m
2 m
1.5 m
5.5 m
5.5 m
FLIGHT TIMELINE

(1) launch, (2) ascent, (3) sides boosters separation, (3.1) sides boosters descent, (3.2) sides boosters parachutes deployment,(4) main booster thrust, (5) hot staging, (5.1) main booster descent, (5.2) main booster parachute deployment, (6) fairing separation, (6.1) fairing descent, (6.2) fairing parachutes deployment, (7) second stage thrust, (8) payload deployment.
DIFFERENT CONFIGURATIONS

Large fairing
small fairing
shuttle
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