Satellite Launch Vehicle Platforms

8 Satellite Launch Vehicle Platforms from 2 Manufacturers meet your specification.
Selected Filters Reset All
  • Manufacturers: SpaceX, Skyrora Ltd
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
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
SKU:SkyHy
Launch Vehicle Diameter:
0.196 m, 0.153 m (second stage)
Payload Capacity:
Up to2 Kg
Number of Stage:
Three-Stage
First Stage Engine Thrust:
7.3 kN
First Stage Engine ISP:
191 Sec
Second Stage Engine Thrust:
1.95 kN
Second Stage Engine ISP:
192 Sec
Propellant:
HTPB
more info
Description:Skylark Micro is a two stage, supersonic rocket powered by solid rocket motors
Launch Vehicle Diameter:
0.102 m, 0.075 m (Second stage)
Payload Capacity:
Up to1 Kg
Number of Stage:
Three-Stage
First Stage Engine Thrust:
1.56 kN
First Stage Engine ISP:
172 Sec
Second Stage Engine Thrust:
0.84 kN
Second Stage Engine ISP:
181 Sec
Propellant:
HTPB
more info
Description:Skylark Nano has attracted its fair share of headlines and news articles.
Launch Vehicle Diameter:
0.102 m
Payload Capacity:
Up to1 Kg
Number of Stage:
Three-Stage
First Stage Engine Thrust:
1526 N (152.6 KG), 1825 N (182.5 KG)
First Stage Engine ISP:
181 Sec
Propellant:
HTPB
more info

FiltersReset All

Launch Vehicle Mass (m)

Apply

Launch Vehicle Diameter (m)

Apply

Launch Vehicle Height (m)

Apply

Payload Capacity (Kg)

Apply

Space Heritage