Minotaur V: Difference between revisions

Browse history interactively ← Previous edit Next edit →Content deleted Content addedVisual WikitextInline

Revision as of 03:19, 7 September 2013 editDaveplot (talk \| contribs)Extended confirmed users4,635 editsmNo edit summaryTag: Visual edit ← Previous edit		Revision as of 03:29, 7 September 2013 edit undoN2e (talk \| contribs)Extended confirmed users, Pending changes reviewers55,706 edits the launch from the MAR spaceport is now history; first Minotaur V flight is off the groundNext edit →
Line 91:		Line 91:
	==Launch pads==		==Launch pads==
	] at the ], ] at the ] (MARS), and ] of the ] are all capable of accommodating the Minotaur V. {{as of\|2013}}, no launches are scheduled from anywhere except at MARS.<ref>{{cite web\|url=http://space.skyrocket.de/doc_lau/minotaur-4.htm\|title=Minotaur-3/-4/-5 (OSP-2 Peacekeeper SLV)\|first=Gunter\|last=Krebs\|publisher=Gunter's Space Page\|accessdate=2013-01-22}}</ref>		] at the ], ] at the ] (MARS), and ] of the ] are all capable of accommodating the Minotaur V. {{as of\|2013}}, no launches are scheduled from anywhere except at MARS.<ref>{{cite web\|url=http://space.skyrocket.de/doc_lau/minotaur-4.htm\|title=Minotaur-3/-4/-5 (OSP-2 Peacekeeper SLV)\|first=Gunter\|last=Krebs\|publisher=Gunter's Space Page\|accessdate=2013-01-22}}</ref>

			==Launch history==
			The initial launch of a Minotaur V occurred on 6 Sep 2013 at 11:27 p.m. EDT from the ] ]. The launch vehicle payload was the ] ] exoatmosphere science spacecraft.

	==References==		==References==
	{~~{reflist~~}}		{Rreflist\|2}}
	{{refbegin}}
	{{refend}}

	{{Expendable launch systems}}		{{Expendable launch systems}}

Revision as of 03:29, 7 September 2013

Template:Launching/Minotaur

Minotaur V
Size

Function	Expendable launch system
Manufacturer	Orbital Sciences
Country of origin	United States
Diameter	1.67 m
Stages	Five
Capacity
Payload to GTO
Mass	532 kg
Payload to TLI
Mass	342 kg

Associated rockets
Family	Minotaur
Launch history
Status	Development
Launch sites	SLC-8, Vandenberg AFB LP-0B, MARS LP-1, Kodiak

First stage – SR-118
Powered by	1 Solid
Maximum thrust	1,607 kilonewtons (361,000 lb_f)
Burn time	83 seconds
Propellant	Solid
Second stage – SR-119
Powered by	1 Solid
Maximum thrust	1,365 kilonewtons (307,000 lb_f)
Burn time	54 seconds
Propellant	Solid
Third stage – SR-120
Powered by	1 Solid
Maximum thrust	329 kilonewtons (74,000 lb_f)
Burn time	62 seconds
Propellant	Solid
Fourth stage – Star-48V
Powered by	1 Solid
Maximum thrust	64 kilonewtons (14,000 lb_f)
Burn time	84 seconds
Propellant	Solid
Fifth stage (Baseline) – Star-37FM
Powered by	1 Solid
Maximum thrust	47.26 kilonewtons (10,620 lb_f)
Burn time	63 seconds
Propellant	Solid
Fifth stage (Optional) – Star-37FMV
Powered by	1 Solid
Propellant	Solid

[edit on Wikidata]

The Minotaur V is an American expendable launch system derived from the Minotaur IV, itself a derivative of the LGM-118 Peacekeeper ICBM. It is being developed by Orbital Sciences Corporation, and is scheduled to make its maiden flight in September 2013 carrying the LADEE spacecraft for NASA.

Design

The Minotaur V is a five stage vehicle, and is designed to place up to 630 kilograms (1,390 lb) of payload into a geosynchronous transfer orbit, or 437 kilograms (963 lb) on a trans-lunar trajectory. It consists of a Minotaur IV+, with a Star-37 as a fifth stage. Two variants are available, one with a spin-stabilized Star-37FM upper stage, and the other with a Star-37FMV capable of three-axis stabilization. The Star-37FMV upper stage is heavier, reducing payload capacity, but is more maneuverable.

Launch pads

Space Launch Complex 8 at the Vandenberg Air Force Base, Pad 0B at the Mid-Atlantic Regional Spaceport (MARS), and Pad 1 of the Kodiak Launch Complex are all capable of accommodating the Minotaur V. As of 2013, no launches are scheduled from anywhere except at MARS.

Launch history

The initial launch of a Minotaur V occurred on 6 Sep 2013 at 11:27 p.m. EDT from the Mid-Atlantic Regional Spaceport launchpad 0B. The launch vehicle payload was the LADEE Lunar exoatmosphere science spacecraft.

References

{Rreflist|2}}

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 6C 7 7A 8 11 11H 12 LVM3 Minotaur I IV V C Nuri OS-M1 Pegasus XL Proton-M PSLV Qaem 100 Qased Shavit 2 Simorgh SLS Block 1 Soyuz-2 2.1a / STA 2.1b / STB 2-1v SSLV Starship Tianlong-2 Unha Vega C Vulcan Centaur Zhuque 2
In development	Antares 330 Bloostar Cyclone-4M Deca Epsilon S Eris Gravity-2 Hyperbola-2 Irtysh Kuaizhou 21 31 Long March 9 10 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 RS1 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 Vega original 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)

v t e Orbital launch systems developed in the United States
Active	Atlas V** Electron Falcon 9 Block 5 Falcon Heavy Firefly Alpha Minotaur I IV V C Pegasus XL SLS Block 1 Vulcan Centaur
In development	Antares 330 Daytona I MLV New Glenn Neutron Nova Red Dwarf SLS Block 1B Block 2 Starship Terran R
Retired	Antares 110/120/130/230/230+ Athena I II Atlas B D E/F G H I II III LV-3B SLV-3 Able Agena Centaur Conestoga Delta A B C D E G J L M N 0100 1000 2000 3000 4000 5000 II III IV IV Heavy Falcon 1 Falcon 9 v1.0 v1.1 v1.2 "Full Thrust" H-I* Juno I Juno II LauncherOne N-I* N-II* Pilot Rocket 3 RS1 Saturn I IB V Scout Space Shuttle SPARK Sparta Terran 1 Thor Able Ablestar Agena Burner Delta DSV-2U Thorad-Agena Titan II GLV IIIA IIIB IIIC IIID IIIE 34D 23G CT-3 IV Vanguard
* - Japanese projects using US rockets or stages ** - uses Russian engines - never succeeded - no new orders accepted - used Ukrainian first stage

This rocketry article is a stub. You can help Misplaced Pages by expanding it.

"Lunar Atmosphere and Dust Environment Explorer (LADEE) Mission website". NASA.
^ "Fact Sheet" (PDF). Minotaur V. Orbital Sciences Corporation. Retrieved 2013-01-22.
Krebs, Gunter. "Minotaur-3/-4/-5 (OSP-2 Peacekeeper SLV)". Gunter's Space Page. Retrieved 2013-01-22.

Categories: