Sparta (rocket)

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Sparta
Size

Has use	Sounding rocket Launch system
Manufacturer	ABMA/Chrysler
Country of origin	United States
Height	21.8 metres (72 ft)
Diameter	1.78 metres (5 ft 10 in)
Mass	30,000 kilograms (66,000 lb)
Stages	3
Capacity
Payload to LEO
Mass	45 kilograms (99 lb)

Associated rockets
Family	Redstone
Comparable	Jupiter-C Juno I
Launch history
Status	Retired
Launch sites	Woomera Test Range
Total launches	10
Success(es)	9
Failure(s)	1
First flight	28 November 1966
Last flight	29 November 1967
People or cargo transported	WRESAT

First stage – Redstone
Powered by	1 A-7
Maximum thrust	416 kilonewtons (94,000 lbf)
Specific impulse	265 sec
Burn time	155 seconds
Propellant	LOX/Ethanol
Second stage –
Powered by	1
Maximum thrust	93 kilonewtons (21,000 lbf)
Specific impulse	293 sec
Burn time	36 seconds
Propellant	Solid
Third stage – BE-3
Powered by	1 solid
Maximum thrust	34
Burn time	9 seconds
Propellant	Solid

The Sparta was a three-stage rocket that launched Australia's first Earth satellite, WRESAT, on 29 November 1967.

Sparta used a surplus American Redstone as its first stage, an as a second stage, and a BE-3 as a third stage. Several Spartas were launched from 1966–67 from Woomera Test Range in Woomera, South Australia as part of a joint United States–United Kingdom–Australian research program aimed at understanding re-entry phenomena, and the U.S. donated a spare for the scientific satellite launch into polar orbit.

The first stage was recovered from the Simpson Desert in 1990 after being found in searches by explorer Dick Smith the previous year.^[1]^: 76–80

Sparta on the pad at Woomera

References[]

^ Douherty, Kevin. "Retrieving Woomera's Heritage" (PDF). Retrieved 3 August 2016. Cite journal requires |journal= (help)

Wade, Mark. "Redstone". Encyclopedia Astronautica. Archived from the original on 2009-04-15. Retrieved 2009-04-07.

v t Orbital launch systems
List of orbital launch systems Comparison of orbital launch systems
Current	Angara A5 Antares 230+ Ariane 5 Atlas V Ceres-1 Delta IV Heavy Electron Epsilon Falcon 9 Block 5 Falcon Heavy Firefly Alpha^† GSLV Mk II Mk III H-IIA Hyperbola-1 Jielong 1 Kuaizhou 1 1A 11^† Kaituozhe 2 LauncherOne Long March 2C 2D 2F 3A 3B/E 3C 4B 4C 5 5B 6 7 7A 8 11 Minotaur I IV V C Nuri^† OS-M1^† Pegasus XL Proton-M PSLV Qased Rocket 3 Shavit 2 Simorgh^† Soyuz-2 2.1a / STA 2.1b / STB 2-1v Unha Vega Zenit 3SL 3SLB 3F Zhuque-1^†
In development	Amur Angara 1.2 Ariane 6 Bloostar Cyclone-4M Eris Firefly Beta H3 Hyperbola-2 Irtysh Kuaizhou 21 31 Long March 921 rocket 9 Miura 5 Neutron New Glenn New Line 1 OS-M 2 4 Orbex Prime Red Dwarf SLS Block 1 Block 1B Block 2 Soyuz-7 SSLV Starship Terran 1 R Vega C E Vulcan Zero Zhuque-2 Zuljanah
Retired	Antares 110 120 130^† 230 Ariane 1 2 3 4 ASLV Athena I II Atlas B D E/F G H I II III LV-3B SLV-3 Able Agena Centaur Black Arrow Conestoga^† Delta A B C D E G J L M N 0100 1000 2000 3000 4000 5000 II III IV Diamant Dnepr Energia Europa^† Falcon 1 Falcon 9 v1.0 v1.1 v1.2 "Full Thrust" Feng Bao 1 GSLV Mk I H-I H-II H-IIB Juno I Juno II Kaituozhe-1 Kosmos 1 2I 3 3M Lambda 4S Long March 1 1D^† 2A 2E 3 3B 4A Mu 4S 3C 3H 3S 3SII V N1^† N-I N-II Naro-1 Paektusan^† Pilot-2^† R-7 Luna Molniya M L Polyot Soyuz original FG L M U U2 Soyuz/Vostok Sputnik Voskhod Vostok L K 2 2M R-29 Shtil' Volna^† Safir 1 1A 1B Saturn I IB V Scout Shavit original Shavit 1 SLV Space Shuttle SPARK^† Sparta SS-520 Start-1 Thor Able Ablestar Agena Burner Delta DSV-2U Thorad-Agena Titan II GLV IIIA IIIB IIIC IIID IIIE 34D 23G CT-3 IV Tsyklon original 2 3 Universal Rocket UR-500 Proton Proton-K Rokot Strela Vanguard VLS-1^† Zenit 2 2M
Classes	Sounding rocket Small-lift launch vehicle Medium-lift launch vehicle Heavy-lift launch vehicle Super heavy-lift launch vehicle
This Template lists historical, current, and future space rockets that at least once attempted (but not necessarily succeeded in) an orbital launch or that are planned to attempt such a launch in the future Symbol ^† indicates past or current rockets that attempted orbital launches but never succeeded (never did or has yet to perform a successful orbital launch)

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