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SPECIFICATIONS
LIFTOF MASS
170 000 KG
LIFTOFF THRUT
2.5 MN
PAYLOAD TO LEO
5 000 KG
PAYLOAD TO SSO
3 200 KG
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)
SECOND STAGE ENGINE
M-30 (×1)
SECOND STAGE ENGINE ARCHITECTURE
ELECTRIC PUMPS
SECOND STAGE ENGINE CAPACITY
290 KN / 350s (vac)
HEIGHT
38 m
DELAY BETWEEN TWO FLIGHT
48 H
REUSABILITY
FIRST STAGE / FAIRING
LAUNCH COST
8 000 000 $
RELEASE DATE
2027 - 2028
OVERVIEW
PAYLOAD
SECOND STAGE TANK (LCH4/LOX)
HOT STAGE RING
GRID FINS
battery / COPV

M-250 (×1)*
FAIRING
M-30 ENGINE (× 1)
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
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
T-5
T-13
T-13

SPECIFICATIONS :
LIFTOF MASS
450 000 KG
LIFTOFF THRUT
7.5 MN
PAYLOAD TO LEO
13 000 KG
PAYLOAD TO SSO
8 300 KG
PAYLOAD TO GTO
4 200 KG
FIRST STAGE ENGINE
M-250 (×3)
FIRST STAGE ENGINE ARCHUTECTURE
GAZ GENERATOR
FIRST STAGE ENGINE CAPACITY
2.5 MN / 315 s (sl)
SECOND STAGE ENGINE
M-30 (×1)
SECOND STAGE ENGINE ARCHITECTURE
ELECTRIC PUMPS
SECOND STAGE ENGINE CAPACITY
290 KN / 350s (vac)
HEIGHT
42 m
DELAY BETWEEN TWO FLIGHT
72 H
REUSABILITY
FIRSTS STAGES / FAIRING
LAUNCH COST
15 000 000 $
RELEASE DATE
2028 - 2029
OVERVIEW

PAYLOAD
SECOND STAGE TANK (LCH4/LOX)
HOT STAGE RING
GRID FINS
COPV
M-250 (×3)*
LEFT BOOSTER
FAIRING
M-30 engine (×1)*
RCS THRUSTER
RIGHT BOOSTER
FIRST STAGE TANK (LCH4/LOX)
DEPLOYABLE HEAT SHEILD
FAIRING DIMENSIONS

5 m
5.5 m
1.25 m
1.5 m
1.25 m
1 m
1.2 m
1 m
3.5 m
3.5 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
Crewed capsule
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