The Minotaur III, also known as OSP-2 Target Launch Vehicle, Peacekeeper TLV or OSP-2 TLV is an American rocket derived from the LGM-118 Peacekeeper missile. It is a member of the Minotaur family of rockets produced by Orbital Sciences Corporation, and is used for long range suborbital launches with heavy payloads. Minotaur III launches will be conducted from Vandenberg Air Force Base and the Kodiak Launch Complex.
| Attributes | Values |
|---|
| rdf:type
| |
| rdfs:label
| - Minotaur III (en)
- Minotaur III (pt)
- Минотавр-3 (ru)
- Minotaur III (sv)
|
| rdfs:comment
| - Минотавр-3 (англ. Minotaur III, OSP-2 TLV, Peacekeeper TLV) — американская военная суборбитальная четырёхступенчатая ракета-носитель среднего класса, также известная как Peacekeeper TLV, разработанная и сконструированная компанией «Орбитальная научная корпорация», на основе тяжелой МБР MX. Ракета-носитель применяется для испытания системы противоракетной обороны (ПРО). (ru)
- Minotaur III är en amerikansk fastbränsleraket under utveckling. Raketen ingår i raketserien Minotaur. (sv)
- The Minotaur III, also known as OSP-2 Target Launch Vehicle, Peacekeeper TLV or OSP-2 TLV is an American rocket derived from the LGM-118 Peacekeeper missile. It is a member of the Minotaur family of rockets produced by Orbital Sciences Corporation, and is used for long range suborbital launches with heavy payloads. Minotaur III launches will be conducted from Vandenberg Air Force Base and the Kodiak Launch Complex. (en)
- O Minotaur III, também conhecido como OSP-2 Target Launch Vehicle, Peacekeeper TLV ou OSP-2 TLV é um foguete Norte americano, derivado do míssil LGM-118 Peacekeeper. Ele é membro da família de foguetes Minotaur produzidos pela Orbital Sciences Corporation e é usado para lançamentos sub-orbitais de cargas úteis pesadas. Os lançamentos do Minotaur III devem ser efetuados a partir da Base da Força Aérea de Vandenberg e do Kodiak Launch Complex. (pt)
|
| foaf:name
| |
| name
| |
| dcterms:subject
| |
| Wikipage page ID
| |
| Wikipage revision ID
| |
| Link from a Wikipage to another Wikipage
| |
| Link from a Wikipage to an external page
| |
| sameAs
| |
| sites
| |
| dbp:wikiPageUsesTemplate
| |
| manufacturer
| |
| status
| |
| stages
| |
| has abstract
| - The Minotaur III, also known as OSP-2 Target Launch Vehicle, Peacekeeper TLV or OSP-2 TLV is an American rocket derived from the LGM-118 Peacekeeper missile. It is a member of the Minotaur family of rockets produced by Orbital Sciences Corporation, and is used for long range suborbital launches with heavy payloads. Minotaur III rockets consist of four stages; the SR-118 first stage, SR-119 second stage and SR-120 third stage of a decommissioned Peacekeeper missile, with a fourth stage, derived from the stage used on Pegasus and Minotaur I rockets. The Minotaur III is capable of launching a 3,000 kilograms (6,600 lb) payload 5,000 kilometres (3,100 mi) downrange on a suborbital trajectory. Minotaur III launches will be conducted from Vandenberg Air Force Base and the Kodiak Launch Complex. (en)
- Минотавр-3 (англ. Minotaur III, OSP-2 TLV, Peacekeeper TLV) — американская военная суборбитальная четырёхступенчатая ракета-носитель среднего класса, также известная как Peacekeeper TLV, разработанная и сконструированная компанией «Орбитальная научная корпорация», на основе тяжелой МБР MX. Ракета-носитель применяется для испытания системы противоракетной обороны (ПРО). (ru)
- Minotaur III är en amerikansk fastbränsleraket under utveckling. Raketen ingår i raketserien Minotaur. (sv)
- O Minotaur III, também conhecido como OSP-2 Target Launch Vehicle, Peacekeeper TLV ou OSP-2 TLV é um foguete Norte americano, derivado do míssil LGM-118 Peacekeeper. Ele é membro da família de foguetes Minotaur produzidos pela Orbital Sciences Corporation e é usado para lançamentos sub-orbitais de cargas úteis pesadas. O foguete Minotaur III consiste de quatro estágios: um SR-118 como primeiro, um SR-119 como segundo e um SR-120 como terceiro, e um Super-HAPS (Hydrazine Auxiliary Propulsion System), como quarto. O Minotaur III é capaz de lançar 3.000 kg num raio de 5.000 km em trajetória sub-orbital. Os lançamentos do Minotaur III devem ser efetuados a partir da Base da Força Aérea de Vandenberg e do Kodiak Launch Complex. (pt)
|
| country-origin
| |
| function
| - Heavy suborbital launch system (en)
|
| launch site
| |
| gold:hypernym
| |
| prov:wasDerivedFrom
| |
| page length (characters) of wiki page
| |
| status
| |
| manufacturer
| |
| foaf:isPrimaryTopicOf
| |
| is Link from a Wikipage to another Wikipage
of | |
| is foaf:primaryTopic
of | |
![[RDF Data]](/fct/images/sw-rdf-blue.png)
![[cxml]](/fct/images/cxml_doc.png)
![[csv]](/fct/images/csv_doc.png)
![[text]](/fct/images/ntriples_doc.png)
![[turtle]](/fct/images/n3turtle_doc.png)
![[ld+json]](/fct/images/jsonld_doc.png)
![[rdf+json]](/fct/images/json_doc.png)
![[rdf+xml]](/fct/images/xml_doc.png)
![[atom+xml]](/fct/images/atom_doc.png)
![[html]](/fct/images/html_doc.png)