About: Triamese

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The Triamese was a 1965 design for an orbital launch system from General Dynamics. This vehicle was composed of three similar winged vehicles. The fuel of each vehicle was used in sequence to feed all of the motors via a manifold. After the vehicle was empty it separated from the remaining active vehicles and returned to earth for a Horizontal recovery. The final stage held the cargo. The overall concept was very similar to the 1964 BAC Mustard design and suffered the same fate.

Property	Value
dbo:abstract	The Triamese was a 1965 design for an orbital launch system from General Dynamics. This vehicle was composed of three similar winged vehicles. The fuel of each vehicle was used in sequence to feed all of the motors via a manifold. After the vehicle was empty it separated from the remaining active vehicles and returned to earth for a Horizontal recovery. The final stage held the cargo. The overall concept was very similar to the 1964 BAC Mustard design and suffered the same fate. (en)
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dbo:wikiPageRevisionID	1120527546 (xsd:integer)
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dcterms:subject	dbc:Rocket-powered_aircraft dbc:Spaceplanes dbc:Cancelled_space_launch_vehicles dbc:Former_proposed_space_launch_system_concepts
rdfs:comment	The Triamese was a 1965 design for an orbital launch system from General Dynamics. This vehicle was composed of three similar winged vehicles. The fuel of each vehicle was used in sequence to feed all of the motors via a manifold. After the vehicle was empty it separated from the remaining active vehicles and returned to earth for a Horizontal recovery. The final stage held the cargo. The overall concept was very similar to the 1964 BAC Mustard design and suffered the same fate. (en)
rdfs:label	Triamese (en)
owl:sameAs	wikidata:Triamese https://global.dbpedia.org/id/GUnny
prov:wasDerivedFrom	wikipedia-en:Triamese?oldid=1120527546&ns=0
foaf:isPrimaryTopicOf	wikipedia-en:Triamese
is dbo:wikiPageWikiLink of	dbr:Douglas_Astro dbr:BAC_Mustard
is foaf:primaryTopic of	wikipedia-en:Triamese

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