M-V
In-activeIHI Corporation (IHI)
Feb. 12, 1997
Description
The M-V rocket also called Mu-5 was a Japanese solid-fuel rocket designed to launch scientific satellites.
Specifications
-
Minimum Stage
3 -
Max Stage
4 -
Length
30.8 m -
Diameter
2.5 m -
Fairing Diameter
2.5 m -
Launch Mass
137.0 T -
Thrust
3780.0 kN
Family
-
Name
M-V -
Family
― -
Variant
V -
Alias
― -
Full Name
M-V
Payload Capacity
-
Launch Cost
― -
Low Earth Orbit
1800.0 kg -
Geostationary Transfer
Orbit
― -
Direct Geostationary
― -
Sun-Synchronous Capacity
―
IHI Corporation
Commercial
None
IHINone
Flight Record
No spaceflights found for .
Falcon 9
TRACERS
Space Launch Complex 4E - Vandenberg SFB, CA, USANASA's Tandem Reconnection and Cusp Electrodynamics Reconnaissance Satellites (TRACERS) mission, consisting of two identical satellites that will orb…
Falcon 9
O3b mPower 9-10
Space Launch Complex 40 - Cape Canaveral SFS, FL, USA2 high-throughput communications satellites in Medium Earth Orbit (MEO) built by Boeing and operated by SES.
Falcon 9
Starlink Group 17-3
Space Launch Complex 4E - Vandenberg SFB, CA, USAA batch of 24 satellites for the Starlink mega-constellation - SpaceX's project for space-based Internet communication system.
Falcon 9
Project Kuiper (KF-01)
Space Launch Complex 40 - Cape Canaveral SFS, FL, USAFirst of a three launches contract for Amazon's Kuiper low Earth orbit satellite internet constellation, with 24 satellites on board.
Falcon 9
Starlink Group 15-2
Space Launch Complex 4E - Vandenberg SFB, CA, USAA batch of 26 satellites for the Starlink mega-constellation - SpaceX's project for space-based Internet communication system.
