Satellite Launch Vehicle Platforms - Page 3

33 Satellite Launch Vehicle Platforms from 12 Manufacturers meet your specification.
Description:With the inaugural launch of our Dauntless vehicle set for 2023, Vaya Space will be equipped to offer launch services to commercial and federal entities
Launch Vehicle Diameter:
2.15 to 2.5 m
Launch Vehicle Height:
35 m
Payload Capacity:
600 to 1000 Kg
Number of Stage:
Single Stage
First Stage Engine:
STAR-3D Engine
more info
SKU:FALCON 9
Launch Vehicle Mass:
549054 Kg
Launch Vehicle Diameter:
3.7 m
Launch Vehicle Height:
70 m
Payload Capacity:
4020 to 22800 Kg
Number of Stage:
Two Stage
First Stage Engine:
Merlin Engine
First Stage Engine Thrust:
845000 N
Second Stage Engine:
Merlin Vaccum Engine
Second Stage Engine Thrust:
981000 N
Propellant:
Kerosene (RP-1), LOX
Space Heritage:
Yes
more info
Description:Falcon Heavy is the most powerful operational rocket in the world by a factor of two. Falcon Heavy can lift more than twice the payload of the next closest operational vehicle, the Delta IV Heavy
Launch Vehicle Mass:
1420788 Kg
Launch Vehicle Diameter:
12.2 m
Launch Vehicle Height:
70 m
Payload Capacity:
16800 to 63800 Kg
Number of Stage:
Two Stage
First Stage Engine:
Merlin Engine
First Stage Engine Thrust:
845000 N
Second Stage Engine:
Merlin Vaccum Engine
Second Stage Engine Thrust:
981000 N
Propellant:
Kerosene (RP-1), LOX
Space Heritage:
Yes
more info
Description:SpaceX’s Starship system represents a fully reusable transportation system designed to service Earth orbit needs as well as missions to the Moon and Mars
Launch Vehicle Diameter:
9 m
Launch Vehicle Height:
50 m
Payload Capacity:
100000 to 150000 Kg
First Stage Engine:
Raptor Engine
First Stage Engine Thrust:
500 klbf
Propellant:
Liquid Methane (CH4), Liquid Oxygen (LOX)
more info
Description:New Glenn is a single configuration heavy-lift launch vehicle capable of carrying people and payloads routinely to Earth orbit and beyond
Launch Vehicle Diameter:
7 m
Launch Vehicle Height:
98 m
Payload Capacity:
13 to 45 metric tons
Number of Stage:
Two Stage
First Stage Engine:
BE-4 Engine
First Stage Engine Thrust:
550000 lbf
Second Stage Engine:
BE-3U Engine
Second Stage Engine Thrust:
160000 lbf
Propellant:
LOX, LNG
more info
Payload Capacity:
560 to 815 Kg
Altitude of Apogee:
500 Km
Altitude of Perigee:
500 km
more info
Payload Capacity:
400 to 595 Kg
Altitude of Apogee:
500 Km
Altitude of Perigee:
500 km
more info
Payload Capacity:
290 to 480 Kg
Altitude of Apogee:
500 Km
Altitude of Perigee:
500 km
more info
Launch Vehicle Diameter:
2.2 m
Payload Capacity:
Up to315 Kg
Number of Stage:
Three-Stage
Propellant:
HTP / KEROSENE
Altitude of Apogee:
200 to 1000 Km
more info
Description:Skylark L is a guided, single-stage, suborbital launch vehicle whereby launch is performed vertically from a fixed launching pad.
Launch Vehicle Diameter:
0.7 m
Payload Capacity:
50 Kg
Number of Stage:
Three-Stage
First Stage Engine Thrust:
31kN (sea level), 35kN ( vacuum)
Altitude of Apogee:
102 Km
more info

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Space Heritage