About: Scout X-2

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Scout X-2 was an American expendable launch system and sounding rocket which was flown twice in 1962. It was a four-stage rocket, based on the earlier Scout X-1, uprated first and third stages. It was a member of the Scout family of rockets. The Scout X-2 used an first stage, instead of the earlier used on the Scout X-1. The third stage was the , a more powerful version of the used on earlier variants of the Scout rocket. The second and fourth stages were the same as those used on the Scout X-1; a Castor 1A and an Altair 1A respectively.

Attributes	Values
rdf:type	Thing mean of transportation Rocket rocket yago:Artifact100021939 yago:Conveyance103100490 yago:Instrumentality103575240 yago:Object100002684 yago:PhysicalEntity100001930 yago:Rocket104099429 yago:Vehicle104524313 yago:Whole100003553
rdfs:label	Scout X-2 (en) Scout X-2 (pl) Scout X-2 (pt)
rdfs:comment	Scout X–2 – amerykańska czterostopniowa rakieta nośna rodziny , całkowicie na paliwo stałe. Występowała w czterech wariantach: * X-2 – podstawowy * X-2 1C – pierwszym członem był Algol 1C, a nie Algol 1D, wersja ta nigdy nie wystartowała * X-2B – ostatnim członem był , a nie Altair 1 * X-2M – ostatnim członem był , a nie Altair 1 (pl) O Scout X-2, foi, ao mesmo tempo, um foguete de sondagem e também um veículo de lançamento descartável.Composto de quatro estágios, foi lançado apenas duas vezes em 1962. Baseado no modelo Scout X-1 ele possuia motores mais potentes no primeiro e no terceiro estágios. Houve duas variantes desse modelo: a Scout X-2B, com apenas um lançamento em 27 de setembro de 1963 e a Scout X-2M, com com apenas três lançamentos,entre maio de 1962 e abril de 1963. (pt) Scout X-2 was an American expendable launch system and sounding rocket which was flown twice in 1962. It was a four-stage rocket, based on the earlier Scout X-1, uprated first and third stages. It was a member of the Scout family of rockets. The Scout X-2 used an first stage, instead of the earlier used on the Scout X-1. The third stage was the , a more powerful version of the used on earlier variants of the Scout rocket. The second and fourth stages were the same as those used on the Scout X-1; a Castor 1A and an Altair 1A respectively. (en)
dcterms:subject	Scout (rocket family) 1962 in spaceflight
Wikipage page ID	17698275 (xsd:integer)
Wikipage revision ID	1120093176 (xsd:integer)
Link from a Wikipage to another Wikipage	Scout (rocket family) Scout X-1 Scout X-2M Encyclopedia Astronautica Vandenberg AFB Space Launch Complex 5 Sounding rocket Scout (rocket family) Apogee 1962 in spaceflight Wallops Flight Facility Wallops Flight Facility Launch Area 3 Solrad 4B Aeronomy Plasma (physics) Vought Expendable launch system Low Earth orbit Point Arguello Solid rocket Castor 1A dbr:Algol_1B dbr:Altair_1A dbr:Antares_1A dbr:X-248A dbr:X-254 dbr:Algol_1D dbr:Antares_2A
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	Scout X-2 Scout X-2 Scout X-2 Scout X-2 Scout X-2
sites	Vandenberg AFB Space Launch Complex 5 Wallops Flight Facility Wallops Flight Facility Launch Area 3 Point Arguello
dbp:wikiPageUsesTemplate	dbt:Infobox_Rocket dbt:Cite_web dbt:Convert dbt:Refbegin dbt:Refend dbt:Reflist dbt:Rocket-stub dbt:Short_description dbt:Infobox_Rocket/Payload dbt:Infobox_Rocket/Stage dbt:Orbital_launch_systems dbt:Scout_rockets
success	1 (xsd:integer)
family	Scout (rocket family)
first	1962-03-29 (xsd:date)
last	1962-04-26 (xsd:date)
manufacturer	Vought
status	Retired (en)
stages	Four (en)
has abstract	Scout X-2 was an American expendable launch system and sounding rocket which was flown twice in 1962. It was a four-stage rocket, based on the earlier Scout X-1, uprated first and third stages. It was a member of the Scout family of rockets. The Scout X-2 used an first stage, instead of the earlier used on the Scout X-1. The third stage was the , a more powerful version of the used on earlier variants of the Scout rocket. The second and fourth stages were the same as those used on the Scout X-1; a Castor 1A and an Altair 1A respectively. The first Scout X-2 was launched on a suborbital flight at 07:27 GMT on 29 March 1962. It flew from Launch Area 3 of the Wallops Flight Facility. The flight carried plasma and aeronomy experiments to an apogee of 6,291 kilometres (3,909 mi), and was successful. The second flight, launched on 26 April, carried the Solrad 4B satellite. It failed to reach orbit. Following this launch, the Scout X-2 was replaced by the upgraded Scout X-2M. (en) Scout X–2 – amerykańska czterostopniowa rakieta nośna rodziny , całkowicie na paliwo stałe. Występowała w czterech wariantach: * X-2 – podstawowy * X-2 1C – pierwszym członem był Algol 1C, a nie Algol 1D, wersja ta nigdy nie wystartowała * X-2B – ostatnim członem był , a nie Altair 1 * X-2M – ostatnim członem był , a nie Altair 1 (pl) O Scout X-2, foi, ao mesmo tempo, um foguete de sondagem e também um veículo de lançamento descartável.Composto de quatro estágios, foi lançado apenas duas vezes em 1962. Baseado no modelo Scout X-1 ele possuia motores mais potentes no primeiro e no terceiro estágios. Houve duas variantes desse modelo: a Scout X-2B, com apenas um lançamento em 27 de setembro de 1963 e a Scout X-2M, com com apenas três lançamentos,entre maio de 1962 e abril de 1963. (pt)
country-origin	United States (en)
fail	1 (xsd:integer)
launches	2 (xsd:integer)
launch site	Wallops Flight Facility Point Arguello
gold:hypernym	System
final flight	1962-04-26 (xsd:date)
maiden flight	1962-03-29 (xsd:date)
prov:wasDerivedFrom	wikipedia-en:Scout_X-2?oldid=1120093176&ns=0
diameter (μ)	1.01 (metre)
height (mm)	25000.0 (millimetre)
mass (kg)	16440.0 (kilogram)
mass (kg)	16440.0 (kilogram)
page length (characters) of wiki page	4043 (xsd:nonNegativeInteger)
diameter (μ)	1.010000 (xsd:double)
failed launches	1 (xsd:nonNegativeInteger)

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