Q22786: Difference between revisions
From Spacefaring
Q22786
Bot: Automated import of articles *** existing text overwritten *** |
Bot: Automated import of articles *** existing text overwritten *** |
||
| Line 1: | Line 1: | ||
{{Page|Athena I|Classes|American expendable launch system|Athena-1 | {{Page|Athena I|Classes|American expendable launch system|Athena-1; LLV; LMLV; Lockheed Launch Vehicle; Lockheed Martin Launch Vehicle}} | ||
Latest revision as of 12:43, 2 September 2025
The Athena I, known as the Lockheed Launch Vehicle (LLV) at the time of its first flight and Lockheed Martin Launch Vehicle (LMLV) at the time of its second flight, was an American small expendable launch system which was used for four launches between 1995 and 2001. It is a member of the Athena family of rockets, along with the larger Athena II.
1995 — 2001
Wikimedia, Wikidata
Athena-1; LLV; LMLV; Lockheed Launch Vehicle; Lockheed Martin Launch Vehicle
mass 66300 kilogram, height 18.9 metre, diameter 2.36 metre, payload mass 360 kilogram, payload mass 820 kilogram,
Lockheed Martin, United States,
Reman, 1990s, Republic of Haiti, 1995, Ekran, Dong Fang Hong 2, Athena, Tarshish, Sweden, Sikh Confederacy, United States, Persia, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, Havilah, Democratic Republic of the Congo, Chinland, Calvinist Republic of Ghent, Ashkenaz,
-
Location: KML, Cluster Map, Maps,
LLV-1 ground test| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|
| commons | image | LLV-1 ground test | Commons | ||
