Castor (rocket stage)

:The Castor 1 was first used for a successful suborbital launch of a Scout X-1 rocket on September 2, 1960.{{cite web | url = http://www.tbs-satellite.com/tse/online/lanc_scout.html | title = TSE - Scout | publisher = The Satellite Encyclopedia}}

:It was {{convert|19.42|ft|m}} long, {{convert|2.6|ft|m}} in diameter, and had a burn time of 27 seconds. Castor 1 stages were also used as strap-on boosters for launch vehicles using Thor first stages, including the Delta D. (A Delta-D was used in 1964 to launch Syncom-3, the first satellite placed in a geostationary orbit.) Castor 1 stages were used in 141 launch attempts of Scout and Delta rockets, only 2 of which were failures. They were also used on some thrust-assisted Thor-Agena launchers. The last launch using a Castor 1 was in 1971.{{cite web | url = http://www.astronautix.com/stages/castor1.htm | title = Castor 1 | publisher = Encyclopedia Astronautica | url-status = dead | archive-url = https://web.archive.org/web/20070407132101/http://astronautix.com/stages/castor1.htm | archive-date = 2007-04-07 }}

:The Castor 2 was an upgraded version of the Castor 1. It was first used on a Scout in 1965, and continued to be used on Scouts until the last Scout launch, in 1994. Castor 2 stages were also used as the strap-on boosters for the Delta E, and for the Japanese-built N-I, N-II and H-I rockets. It retained the same diameter as the Castor 1, and was from 5.96 m to 6.27 m in length.

:The Castor 4, along with its A and B variants, were expanded to 1.02 m in diameter. They were used as strap-ons on some Delta, Delta II, Atlas IIAS, and Athena RTV launch vehicles. They were also planned to serve as the first stage of the Spanish Capricornio booster, however, no such flights occurred before the project was cancelled.

:Castor 4B is used in the European Maxus Programme, with launches from Esrange in Sweden.

: Certain versions of the H-IIA rockets flown by JAXA used either two or four strap-on boosters developed and produced by Alliant Techsystems. These boosters use motors which are modified versions of the Castor 4A-XL motor design. These motors are {{convert|38|ft|1}} long and roughly {{convert|40|in|m|2}} in diameter.{{cite web |url=https://www.northropgrumman.com/Capabilities/PropulsionSystems/Documents/NGIS_MotorCatalog.pdf |title=NGIS Propulsion Products Catalog |publisher=NGIS}}

: File:Castor 30 test fire.jpgThe CASTOR 30 motor is based on the CASTOR 120 motor, which has flown on the Taurus I, Athena I and Athena II launch vehicles. The inaugural flight of the new motor occurred in April 2013 as the second stage on the Orbital Sciences Antares medium-lift rocket for International Space Station resupply missions.

: The CASTOR 30 upper stage measures {{convert|138|inch|m}} in length and {{convert|92|inch|m}} in diameter, and it weighs {{convert|30000|lb|kg}}. The motor is nominally designed as an upper stage that can function as a second or third stage as well, depending on the vehicle configuration.

: The CASTOR 30XL solid rocket motor measures {{convert|236|inch|m}} in length and {{convert|92|inch|m}} in diameter, and it weighs approximately {{convert|56000|lb|kg}}. The nozzle is eight feet long with a submerged design with a high performance expansion ratio (56:1) and a dual density exit cone.

Image:Castor 120 for OCO.jpg rocket for the OCO launch]]

:An unrelated development to the earlier Castor 1, 2 and 4, the Castor 120 is a derivative of the first-stage motor of the MX ("Peacekeeper") missile. "120" refers to the planned weight, in thousands of pounds, of the booster at project inception. The actual product turned out lighter than this, however. It was first used as the first-stage motor of Lockheed Martin's Athena I, and later the first and second stages of Athena II.{{cite web | url = http://www.spaceandtech.com/spacedata/motors/castor120_sum.shtml | title = Castor 120 | publisher = Andrews Space & Technology| url-status = usurped |archive-url = https://web.archive.org/web/20120904064934/http://www.spaceandtech.com/spacedata/motors/castor120_sum.shtml|archive-date = September 4, 2012}} After a test launch in August 1995, the first launch of a customer payload took place on August 22, 1997, when an Athena was used to launch the NASA Lewis satellite.

{{cite web | url = http://www-pao.ksc.nasa.gov/kscpao/release/1999/30-99.htm | title = Athena | publisher = NASA | url-status = dead | archive-url = https://web.archive.org/web/20061004180947/http://www-pao.ksc.nasa.gov/kscpao/release/1999/30-99.htm | archive-date = 2006-10-04 }} In 2006 Orbital Sciences Corporation agreed to pay $17.5 million for the Castor 120 motors used in the Taurus XL launch vehicles for the Orbiting Carbon Observatory and Glory satellites.{{cite web |url=http://www.atk.com/news-releases/atk-receives-17-5-million-contract-for-castor-120-motors/ |title=ATK Receives $17.5 Million Contract for CASTOR 120 Motors |publisher=ATK |date=October 23, 2006}} The main solid rocket boosters (SRB-A) of the Japanese H-IIA launch vehicle are based on the Castor 120, and were jointly designed by ATK and IHI Aerospace.{{cite web |url=http://www.atk.com/news-releases/atk-composite-technology-supports-maiden-flight-of-japans-h-iia-space-launch-vehicle/|title=ATK Composite Technology Supports Maiden Flight of Japan's H-IIA Space Launch Vehicle |publisher=ATK |date=August 29, 2001| archive-url=https://web.archive.org/web/20131226092036/http://www.atk.com/news-releases/atk-composite-technology-supports-maiden-flight-of-japans-h-iia-space-launch-vehicle/ |archive-date=2013-12-26}}

Instead of using a D6AC steel case and PBAN binder like the Space Shuttle SRB, these will use the technology derived from the GEM motors which have carbon composite cases and HTPB binder.{{Cite web|url=http://www.spaceflightinsider.com/organizations/nasa/one-on-one-with-atks-charlie-precourt-about-composite-materials-and-nasas-space-launch-system/|title=One-on-One with ATK's Charlie Precourt about composite materials and NASA's Space Launch System|date=7 December 2013}} The carbon composite design eliminates the factory joint common on all Space Shuttle SRBs.

: The CASTOR 300 motor is a proposed booster based on the Space Shuttle Solid Rocket Booster and was intended to be used as the second stage of the OmegA. The inaugural flight of the new motor was suggested to occur as soon as 2021.{{cite web|url=https://spaceflightnow.com/2016/05/27/details-of-orbital-atks-proposed-heavy-launcher-revealed/|title=Details of Orbital ATK's proposed heavy launcher revealed – Spaceflight Now|website=spaceflightnow.com|access-date=13 April 2018}}

: Based on a 1-segment Space Shuttle SRB, the Castor 300 measures {{convert|499.6|inch|m}} in length and {{convert|146.1|inch|m}} in diameter, and it weighs approximately {{convert|300000|lb|kg}}.{{cite web|url=https://www.orbitalatk.com/flight-systems/propulsion-systems/GEM-strapon-booster-system/docs/orbital_atk_motor_catalog_(2012).pdf|title=Orbital ATK|website=www.orbitalatk.com|access-date=13 April 2018}}

: The CASTOR 600 motor is a proposed booster based on the Space Shuttle Solid Rocket Booster and was intended to be used as the first stage of the OmegA's small configurations. The inaugural flight of the new motor was suggested to occur as soon as 2021.

: Based on a 2-segment Space Shuttle SRB, the Castor 600 measures {{convert|860|inch|m}} in length and {{convert|146.1|inch|m}} in diameter, and it weighs approximately {{convert|600000|lb|kg}}.

: The CASTOR 1200 motor is a proposed booster based on the Space Shuttle Solid Rocket Booster and was intended to be used as the first stage of the OmegA's heavy configuration. The inaugural flight of the new motor was suggested to occur in the 2020s. It has also been proposed to replace the 5 segment RSRMVs on the Block 2 Space Launch System.

: Based on a 4-segment Space Shuttle SRB, the Castor 1200 measures {{convert|1476.3|inch|m}} in length and {{convert|146.1|inch|m}} in diameter, and it weighs approximately {{convert|1200000|lb|kg}}.

{{Commons category|Castor (rocket stage)}}

• Antares (rocket), launch vehicle by Northrop Grumman Corporation using Castor 30
• Atlas II
• Graphite-Epoxy Motor
• Little Joe
• Minotaur-C, launch vehicle by Northrop Grumman Corporation using Castor 120
• Thrust Augmented Thor
• Maxus, a European microgravity programme using Castor 4B
• Athena (rocket family)
• Strypi (used Castor as second stage)

{{Reflist}}

{{Upper stages}}

{{Rocket engines}}

{{Suborbital rocket engines}}

{{Use American English|date=January 2014}}

Category:Rocket stages

Category:Solid-fuel rockets

Category:Alliant Techsystems