About: RM-89 Blue Scout I

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The RM-89 Blue Scout I was an American sounding rocket which was flown four times between January 1961 and April 1962. It was used for two test flights, and a flight to investigate atmospheric re-entry. It was a member of the Scout family of rockets. The first two launches was successful, however recovery of the payload failed. The second two launches failed due to problems with the Blue Scout. The Blue Scout II was a four-stage derivative of the Blue Scout I. It was flown four times in 1961, twice with HETS payloads, and twice with the Mercury-Scout 1 satellite.

Attributes	Values
rdf:type	Thing person mean of transportation Rocket rocket yago:Artifact100021939 yago:Conveyance103100490 yago:Instrumentality103575240 yago:Object100002684 yago:PhysicalEntity100001930 yago:Rocket104099429 yago:Vehicle104524313 yago:Whole100003553
rdfs:label	RM-89 Blue Scout I (en) Blue Scout I (pt)
rdfs:comment	The RM-89 Blue Scout I was an American sounding rocket which was flown four times between January 1961 and April 1962. It was used for two test flights, and a flight to investigate atmospheric re-entry. It was a member of the Scout family of rockets. The first two launches was successful, however recovery of the payload failed. The second two launches failed due to problems with the Blue Scout. The Blue Scout II was a four-stage derivative of the Blue Scout I. It was flown four times in 1961, twice with HETS payloads, and twice with the Mercury-Scout 1 satellite. (en) O Blue Scout I - XRM-89, é um foguete de sondagem da Força Aérea dos Estados Unidos. Ele fazia parte da família de foguetes Scout. O programa Blue Scout, era uma variante da Aeronáutica sobre o projetodo foguete Scout da NASA. Também conhecido como HETS de (Hyper Environmental Test System) ou sistema 609A, sendo os foguetes, genericamente conhecidos comoBlue Scout. Diferente da NASA, que usava a Ling-Temco-Vought (LTV) como empresa integradora, a USAF preferiuoptar pela Ford Aeronutronics. (pt)
foaf:depiction
dcterms:subject	Scout (rocket family) 1961 in spaceflight 1962 in spaceflight
Wikipage page ID	23291284 (xsd:integer)
Wikipage revision ID	1088241051 (xsd:integer)
Link from a Wikipage to another Wikipage	Cape Canaveral Air Force Station Cape Canaveral Air Force Station Launch Complex 18 Scout (rocket family) Scout X-1 Sounding rocket Scout (rocket family) 1961 in spaceflight 1962 in spaceflight Plasma (physics) Mercury-Scout 1 RM-90 Blue Scout II Vought Solid rocket Suborbital Castor 1A Atmospheric re-entry dbr:Algol_1B dbr:Antares_1A dbr:HETS_A1 dbr:Hyper_Environmental_Test_System dbr:X-254
Link from a Wikipage to an external page	http://www.designation-systems.net/dusrm/app3/lv-1.html%7Ctitle=LTV http://space.skyrocket.de/doc_lau_fam/scout.htm%7Ctitle=Scout%7Clast=Krebs%7Cfirst=Gunter%7Cpublisher=Gunter's http://www.astronautix.com/lvs/scout.htm%7Carchive-url=https:/web.archive.org/web/20080917030602/http:/www.astronautix.com/lvs/scout.htm%7Curl-status=dead%7Carchive-date=September http://planet4589.org/space/lvdb/launch/Scout%7Ctitle=Scout%7Clast=McDowell%7Cfirst=Jonathan%7Cwork=Orbital
sameAs	RM-89 Blue Scout I RM-89 Blue Scout I RM-89 Blue Scout I RM-89 Blue Scout I RM-89 Blue Scout I
sites	Cape Canaveral Air Force Station Cape Canaveral Air Force Station Launch Complex 18
dbp:wikiPageUsesTemplate	dbt:Infobox_Rocket dbt:Cite_web dbt:Convert dbt:Refbegin dbt:Refend dbt:Reflist dbt:Short_description dbt:USAF_missiles dbt:Infobox_Rocket/Stage dbt:Scout_rockets
thumbnail	wiki-commons:Special:FilePath/Blue_Scout.jpg?width=300
success	2 (xsd:integer)
caption	Blue Scout D6 ahead of the second HETS launch (en)
family	Scout (rocket family)
first	1961-01-07 (xsd:date)
last	1962-04-12 (xsd:date)
manufacturer	Vought
status	Retired (en)
stages	Three (en)
has abstract	The RM-89 Blue Scout I was an American sounding rocket which was flown four times between January 1961 and April 1962. It was used for two test flights, and a flight to investigate atmospheric re-entry. It was a member of the Scout family of rockets. The Blue Scout I was a four-stage rocket derived from the Scout X-1. All four launches occurred from Launch Complex 18B at the Cape Canaveral Air Force Station. The first two launches were conducted on 7 January and 9 May 1961 respectively. They both carried plasma research experiments on suborbital trajectories. The second two launches were conducted on 12 April 1962, with a payload that was intended to investigate atmospheric reentry. The first two launches was successful, however recovery of the payload failed. The second two launches failed due to problems with the Blue Scout. The Blue Scout II was a four-stage derivative of the Blue Scout I. It was flown four times in 1961, twice with HETS payloads, and twice with the Mercury-Scout 1 satellite. (en) O Blue Scout I - XRM-89, é um foguete de sondagem da Força Aérea dos Estados Unidos. Ele fazia parte da família de foguetes Scout. O programa Blue Scout, era uma variante da Aeronáutica sobre o projetodo foguete Scout da NASA. Também conhecido como HETS de (Hyper Environmental Test System) ou sistema 609A, sendo os foguetes, genericamente conhecidos comoBlue Scout. Diferente da NASA, que usava a Ling-Temco-Vought (LTV) como empresa integradora, a USAF preferiuoptar pela Ford Aeronutronics. Usando combinações de estágios diferentes, a USAF criou algumas configurações específicas, sendo uma delas, o Blue Scout I, de três estágios, que omitia oquarto estágio Altair do foguete Scout original. Desse modelo, apenas três lançamento foram efetuados: um em 7 de janeiro de 1961 bem sucedido e outrosdois em maio de 1961 e abril de 1962, ambos resultando em falha e encerrando a vida útil desse modelo. (pt)
country-origin	United States (en)
derivatives	RM-90 Blue Scout II
fail	2 (xsd:integer)
function	Sounding rocket
launches	4 (xsd:integer)
launch site	Cape Canaveral Air Force Station
rocket function	Sounding rocket
gold:hypernym	American
final flight	1962-04-12 (xsd:date)
maiden flight	1961-01-07 (xsd:date)
prov:wasDerivedFrom	wikipedia-en:RM-89_Blue_Scout_I?oldid=1088241051&ns=0
diameter (μ)	1.02 (metre)
height (mm)	21650.0 (millimetre)
mass (kg)	16738.0 (kilogram)
mass (kg)	16738.0 (kilogram)
page length (characters) of wiki page	4193 (xsd:nonNegativeInteger)
diameter (μ)	1.020000 (xsd:double)
failed launches	2 (xsd:nonNegativeInteger)
height (μ)	21.650000 (xsd:double)
mass (g)	16738000.000000 (xsd:double)
status	Retired
successful launches	2 (xsd:nonNegativeInteger)
total launches	4 (xsd:nonNegativeInteger)
manufacturer	Vought

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