Launch Vehicle Platforms

25 Launch Vehicle Platforms for Space Applications from 10 manufacturers listed on SatNow

Launch Vehicle Platforms for space applications from multiple manufacturers are listed on SATNow. Use the filters to select products based on your requirement. View product details, download datasheets, compare products, get quotes and pricing for matching products. SATNow has compiled this list of products specifically for Space and Satellite Applications.

Description:Falcon 9 is a reusable, two-stage rocket designed and manufactured by SpaceX for the reliable and safe transport of people and payloads into Earth orbit and beyond
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: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
Description:H2A202 launch vehicle is a high-performance rocket consist of first stage, second stage, fairing, one or two pairs of solid rocket boosters
Launch Vehicle Mass:
289 Metric Tons
Launch Vehicle Height:
53 m
Number of Stage:
Two Stage
First Stage Engine:
LE-7A Engine
First Stage Engine Thrust:
1098000 N
First Stage Engine ISP:
440 Seconds
Second Stage Engine:
LE-5B Engine
Second Stage Engine Thrust:
137000 N
Second Stage Engine ISP:
448 Seconds
Booster:
Solid Rocket Booster - A
Space Heritage:
Yes
more info
Description:Electron is designed to deliver small satellites to precise and unique orbits
Launch Vehicle Mass:
13000 Kg
Launch Vehicle Diameter:
1.2 m/3.9 ft
Launch Vehicle Height:
18 m/59 ft
Payload Capacity:
200 Kg
Number of Stage:
Three Stage
First Stage Engine:
9 Sea-level Rutherford Engine
First Stage Engine Thrust:
190000 N
First Stage Engine ISP:
311 Seconds
Second Stage Engine:
Single Vacuum Rutherford Engine
Second Stage Engine Thrust:
25800 N
Second Stage Engine ISP:
343 Seconds
Propellant:
LOX, Kerosene
Space Heritage:
Yes
more info
Description:Trailblazer allows the payload to be externally deployed
Launch Vehicle Mass:
452 Kg
Launch Vehicle Diameter:
0.31 m
Launch Vehicle Height:
6.5 m
Payload Capacity:
20 Kg
Number of Stage:
Single Stage
First Stage Engine:
AO-H1 Engine
First Stage Engine Thrust:
9500 N
Second Stage Engine Thrust:
14000 N
Propellant:
Hypergolic Green Propellant
Inclination:
85 Degrees
Altitude of Apogee:
130 Km
more info
Description:Ariane 5 is capable of carry payloads weighing more than 10 metric tons to GTO
Launch Vehicle Mass:
780 Kg
Launch Vehicle Diameter:
5.4 m
Launch Vehicle Height:
50.5 m
Payload Capacity:
10000 Kg
Number of Stage:
Two Stage
First Stage Engine:
Cryogenic Engine
Inclination:
6 Degrees
Altitude of Apogee:
35.943 Km
Altitude of Perigee:
250 Km
Space Heritage:
Yes
more info
Description:The enhanced performance provided by the commercial Proton Launch Vehicle enables our customers to design and launch heavier and more capable spacecraft while maintaining cost effective mission life t...
Launch Vehicle Mass:
705000 Kg
Launch Vehicle Diameter:
4.1
Launch Vehicle Height:
56.2 to 58.2 m
Payload Capacity:
6270 to 6470 Kg
Number of Stage:
Three Stage
First Stage Engine:
RD-276 Liquid Rocket Engines
First Stage Engine Thrust:
10 MN
Second Stage Engine:
RD-0210 Liquid Rocket Engine, RD-0211 Liquid Rocke...
Second Stage Engine Thrust:
2.4 MN
Propellant:
Nitrogen Tetroxide (N2O4) Unsymmetrical DiMethyl H...
Space Heritage:
Yes
more info
Description:Atlas V 400 Series uses a standard common core booster, a Centaur upper stage in a single or dual-engine configuration
Payload Capacity:
1935 to 13250 Kg
Number of Stage:
Two Stage
First Stage Engine:
RD 180 Engine
First Stage Engine Thrust:
860300 lbs
First Stage Engine ISP:
311 Seconds
Second Stage Engine:
RL10 Engine
Second Stage Engine Thrust:
22900 lbs
Second Stage Engine ISP:
450.5 Seconds
Propellant:
Liquid Oxygen, Liquid Kerosene, Liquid Hydrogen
Booster:
Aerojet Rocketdyne Solid Rocket Booster
Inclination:
0 Degrees (GEO), 27 Degrees (GTO), 28.7 Degrees (L...
Space Heritage:
Yes
more info
Description:MIURA 1 is a suborbital launch vehicle, privately developed in Europe. The first space system is fully designed by PLD Space to take your payloads into space and bring them back safely
Launch Vehicle Diameter:
0.7 m
Launch Vehicle Height:
12.5 m
Payload Capacity:
100 Kg
Number of Stage:
Single Stage
First Stage Engine:
TEPREL-B Liquid Bi-propellant Engine
First Stage Engine Thrust:
30000 N
Propellant:
Kerosene, LOX
Altitude of Apogee:
150 Km
more info
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


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