About: N-I

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An Entity of Type : owl:Thing, within Data Space : platform.yourdatastories.eu:8890 associated with source document(s)

The N-I or N-1 was a derivative of the American Delta rocket, produced under licence in Japan. It used a Thor-ELT first stage, a Mitsubishi Heavy Industries-designed LE-3 engine was used as a second stage, and three Castor SRMs. Seven were launched between 1975 and 1982, before it was replaced by the N-II.

Attributes	Values
rdfs:comment	The N-I or N-1 was a derivative of the American Delta rocket, produced under licence in Japan. It used a Thor-ELT first stage, a Mitsubishi Heavy Industries-designed LE-3 engine was used as a second stage, and three Castor SRMs. Seven were launched between 1975 and 1982, before it was replaced by the N-II.
foaf:name	N-I
foaf:depiction
diameter (μ)	2(xsd:double)
final flight	1982-09-03(xsd:dateTime)
height (μ)	34(xsd:double)
launch site	Tanegashima
maiden flight	1975-09-09(xsd:dateTime)
manufacturer	Mitsubishi Heavy Industries, Ltd. McDonnell Douglas Corporation
mass (g)	131330000(xsd:double)
partial failed launches	1(xsd:integer)
rocket function	dbpedia:Launch_vehicle
number of rocket stages	2(xsd:integer) 3(xsd:integer)
status	Retired
successful launches	6(xsd:integer)
thumbnail	http://commons.wikimedia.org/wiki/Special:FilePath/N-I.svg?width=300
total launches	7(xsd:integer)
is differentFrom of	dbpedia:Delta_N
is maiden flight rocket of	dbpedia:1975_in_spaceflight

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