Q907608: Difference between revisions
From Spacefaring
Q907608
Bot: Automated import of articles |
Bot: Automated import of articles *** existing text overwritten *** |
||
| (One intermediate revision by the same user not shown) | |||
| Line 1: | Line 1: | ||
{{Page|Minotaur IV|Classes|active expendable launch system derived from the LGM-118 Peacekeeper ICBM}} | {{Page|Minotaur IV|Classes|active expendable launch system derived from the LGM-118 Peacekeeper ICBM|Minotaur IV Lite; Minotaur IV+; OSP-2 PK; Peacekeeper SLV}} | ||
Latest revision as of 12:48, 2 September 2025
Minotaur IV, also known as Peacekeeper SLV and OSP-2 PK is an active expendable launch system derived from the retired LGM-118 Peacekeeper ICBM. It is operated by Northrop Grumman Space Systems, and made its maiden flight on 22 April 2010 carrying the HTV-2a Hypersonic Test Vehicle. The first orbital launch occurred on 26 September 2010 with the SBSS satellite for the United States Air Force.
Wikimedia, Wikidata
Minotaur IV Lite; Minotaur IV+; OSP-2 PK; Peacekeeper SLV
Orbital Sciences Corporation, United States,
Sikh Confederacy, Republic of Haiti, Minotaur, FASTRAC, Ekran, Dong Fang Hong 2, RAX, O/OREOS, Tarshish, United States, Persia, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, Havilah, Chinland, Calvinist Republic of Ghent, Ashkenaz,
-
Location: KML, Cluster Map, Maps,
| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|