Minotaur IV
ActiveOrbital Sciences Corporation (OSC)
Sept. 27, 2011
Description
The Minotaur IV+ launch system is derived from the Peacekeeper ICBM. The first three stages are taken directly from decommissioned Peacekeeper missiles. It is similar to the Minotaur IV, but uses a larger Star-48V upper stage in place of the Orion-38 used on the baseline Minotaur IV.
Specifications
-
Stages
4 -
Length
23.9 m -
Diameter
2.35 m -
Fairing Diameter
― -
Launch Mass
86.0 T -
Thrust
2200.0 kN -
Apogee (Sub-Orbital)
500.0 km
Family
-
Name
Minotaur IV -
Family
― -
Variant
+ -
Alias
Peacekeeper SLV -
Full Name
Minotaur IV+
Payload Capacity
-
Launch Cost
― -
Low Earth Orbit
1950.0 kg -
Geostationary Transfer
Orbit
― -
Direct Geostationary
― -
Sun-Synchronous Capacity
―
Orbital Sciences Corporation
Commercial
None
OSCKinetica 2
SpaceSail Polar Group #17
Launch Area 140 - Jiuquan Satellite Launch Center, People's Republic of China18 Low Earth Orbit communication satellites with Ku, Q and V band payloads for the G60 constellation operated by Shanghai Spacesail Technologies with…
Electron
The Sea God Surveys (iQPS Launch 9)
Rocket Lab Launch Complex 1A - Rocket Lab Launch Complex 1, Mahia Peninsula, New ZealandSynthetic aperture radar Earth observation satellite for Japanese Earth imaging company iQPS.
Falcon 9
Starlink Group 15-18
Space Launch Complex 4E - Vandenberg SFB, CA, USAA batch of 27 satellites for the Starlink mega-constellation - SpaceX's project for space-based Internet communication system.
GSLV Mk II
IRNSS-1L (NVS-03)
Satish Dhawan Space Centre Second Launch Pad - Satish Dhawan Space Centre, IndiaThis is a replacement satellite for the Indian Regional Navigation Satellite System. The constellation will provide India with an alternative to GPS …
Falcon 9
Starlink Group 15-16
Space Launch Complex 4E - Vandenberg SFB, CA, USAA batch of 27 satellites for the Starlink mega-constellation - SpaceX's project for space-based Internet communication system.
