Sparta (rocket): Difference between revisions

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Sparta
Size

Function	Sounding rocket Launch system
Manufacturer	ABMA/Chrysler
Country of origin	Vereinigte Staaten
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 LA-8
Total launches	10
Success(es)	9
Failure(s)	1
First flight	28 November 1966
Last flight	29 November 1967
Type of passengers/cargo	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/Hydyne
Second stage – Antares-2
Powered by	1 X-259
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

[edit on Wikidata]

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

Sparta used a surplus American Redstone as its first stage, an Antares as a second stage 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.

References

Wade, Mark. "Redstone". Encyclopedia Astronautica. Retrieved 2009-04-07.

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v t e Orbital launch systems
List of orbital launch systems Comparison of orbital launch systems
Current	Angara 1.2 A5 Ariane 6 Atlas V Ceres 1 1S Chollima-1 Electron Falcon 9 Block 5 Falcon Heavy Firefly Alpha Gravity-1 GSLV H-IIA H3 Hyperbola-1 Jielong 1 3 KAIROS^† Kaituozhe 2 Kinetica 1 Kuaizhou 1 1A 11 Long March 2C 2D 2F 3A 3B/E 3C 4B 4C 5 5B 6 6A 7 7A 8 11 11H LVM3 Minotaur I IV V C Nuri OS-M1^† Pegasus XL Proton-M PSLV Qaem 100 Qased RS1^† Shavit 2 Simorgh SLS Block 1 Soyuz-2 2.1a / STA 2.1b / STB 2-1v SSLV Starship Tianlong-2 Unha Vega original C Vulcan Centaur Zhuque 2
In development	Antares 330 Bloostar Cyclone-4M Epsilon S Eris Gravity-2 Hyperbola-2 Irtysh Kuaizhou 21 31 Long March 9 10 12 Miura 5 MLV Neutron New Glenn New Line 1 NGLV Nova OS-M 2 4 Orbex Prime Pallas-1 Red Dwarf SLS Block 1B Block 2 Soyuz-7 Terran R Tianlong-3 VLM Vega E Zero Zhuque 3 Zuljanah
Retired	Antares 110 120 130^† 230 230+ Ariane 1 2 3 4 5 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 IV Heavy Diamant Dnepr Energia Epsilon Europa I^† II^† 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 original 1 2/2I 3 3M Lambda 4S LauncherOne 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^† Rocket 3 Safir 1 1A 1B Saturn I IB V Scout X-1 Blue Scout II^† X-2^† X-2M X-3 X-3M X-4 X-2B^† B A B-1 D-1 A-1 E-1 F-1 G-1 Shavit original 1 SLV Space Shuttle SPARK^† Sparta SS-520 Start-1 Terran 1^† Thor Able Ablestar 1 2 Agena A B D Burner 1 2 Delta DSV-2U Thorad-Agena SLV-2G SLV-2H Titan II GLV IIIA IIIB IIIC IIID IIIE 34D 23G CT-3 IV Tsyklon R-36-O original 2 3 Universal Rocket UR-500 Proton Proton-K Rokot Strela Vanguard VLS-1^† Zenit 2 2M 2FG 3SL 3SLB 3F Zhuque 1^†
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)

@@ Line 5: / Line 5: @@
 |caption =
 |name           =  Sparta
-|function       =  Sounding rocket<br/>Launch System
+|function       =  Sounding rocket<br/>Launch system
 |manufacturer   =  [[ABMA]]/[[Chrysler]]
 |country-origin =  {{USA}}
@@ Line 11: / Line 11: @@
 |diameter     =  {{convert|1.78|m}}
 |mass         =  {{convert|30000|kg}}
-|stages       =  Three
+|stages       =  3
 |capacities =
   {{Infobox Rocket/Payload

Revision as of 03:43, 28 October 2010

References