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RESILIENT SPACE TECHNOLOGIES
Innovative engineering for reusable, cost-efficient spaceflight.
SUBORBITAL LAUNCHER
ORBITAL LAUNCHERS
T-5
THE T-5 IS A SMALL TWO-STAGE, REUSABLE, ORBITAL-CLASS LAUNCH VEHICLE. IT IS DESIGNED FOR SMALLSATS, CONSTELLATIONS BUT ALSO FOR SMALL UNMANNED SPACE PLANES.
RAPID OVERVIEW
PAYLOAD TO LEO
5 000 KG
PAYLOAD TO GTO
1 500 KG
PROPELLANT
LCH4 / LOX
REUSABILITY
FIRST STAGE / FAIRING
COST PER LAUNCHS
6 000 000 $
FIRST LAUCH DATE
2027 -2028
T-13
The T-14 is a HEAVY version of the T-5. Thanks to its two side thrusters, it can carry heavier satellites, but also perform manned flights.
RAPID OVERVIEW
PAYLOAD TO LEO
13 000 KG
PAYLOAD TO GTO
4 200 KG
PROPELLANT
LCH4 / LOX
REUSABILITY
FIRST STAGE / FAIRING
COST PER LAUNCHS
15 000 000 $
FIRST LAUCH DATE
2028 -2029
T-30
The T-30 is a high-capacity, two-stage reusable orbital launch vehicle. It is designed for medium/heavy satellites, large constellations, space station modules, small spaceplanes, or orbital refueling.
RAPID OVERVIEW
PAYLOAD TO LEO
30 000 KG
PAYLOAD TO GTO
10 000 KG
PROPELLANT
LCH4 / LOX
REUSABILITY
FIRST STAGE / FAIRING
COST PER LAUNCHS
25 000 000 $
FIRST LAUCH DATE
2032 -2033
T-70
The T-70 is a heavy version of the T-30. It is designed for heavy satellites, high-energy orbits, refueling, space station modules or unmanned lunar missions.
RAPID OVERVIEW
PAYLOAD TO LEO
70 000 KG
PAYLOAD TO GTO
24 300 KG
PROPELLANT
LCH4 / LOX
REUSABILITY
FIRST STAGE / FAIRING
COST PER LAUNCHS
55 000 000 $
FIRST LAUCH DATE
2033 -2034
T-150
The T-150 is a reusable, two-stage super-heavy launcher. It is designed for giant satellites, space stations, orbital refueling, or crewed lunar missions.
RAPID OVERVIEW
PAYLOAD TO LEO
150 000 KG
PAYLOAD TO GTO
52 000 KG
PROPELLANT
LCH4 / LOX
REUSABILITY
FIRST STAGE / FAIRING
COST PER LAUNCHS
120 000 000 $
FIRST LAUCH DATE
> 2035
T-350
The T-350 is a heavy version of the T-150. It is designed for heavier orbital infrastructure, heavy refueling or crewed interplanetary missions.
RAPID OVERVIEW
PAYLOAD TO LEO
350 000 KG
PAYLOAD TO GTO
120 000 KG
PROPELLANT
LCH4 / LOX
REUSABILITY
FIRST STAGE / FAIRING
COST PER LAUNCHS
280 000 000 $
FIRST LAUCH DATE
> 2035
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