Minotaur V: Difference between revisions
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==Launch pads== |
==Launch pads== |
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[[Vandenberg AFB Space Launch Complex 8|Space Launch Complex 8]] at the [[Vandenberg Air Force Base]], [[Mid-Atlantic Regional Spaceport Launch Pad 0|Pad 0B]] at the [[Mid-Atlantic Regional Spaceport]] (MARS), and [[Kodiak Launch Complex Pad 1|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.<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> |
[[Vandenberg AFB Space Launch Complex 8|Space Launch Complex 8]] at the [[Vandenberg Air Force Base]], [[Mid-Atlantic Regional Spaceport Launch Pad 0|Pad 0B]] at the [[Mid-Atlantic Regional Spaceport]] (MARS), and [[Kodiak Launch Complex Pad 1|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.<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> |
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==Launch history== |
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The initial launch of a Minotaur V occurred on 6 Sep 2013 at 11:27 p.m. EDT from the [[Mid-Atlantic Regional Spaceport]] [[Mid-Atlantic Regional Spaceport Launch Pad 0|launchpad 0B]]. The launch vehicle payload was the [[LADEE]] [[Lunar]] exoatmosphere science spacecraft. |
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==References== |
==References== |
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{{Expendable launch systems}} |
{{Expendable launch systems}} |
Revision as of 03:29, 7 September 2013
Function | Expendable launch system |
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Manufacturer | Orbital Sciences |
Country of origin | United States |
Size | |
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 lbf) |
Burn time | 83 seconds |
Propellant | Solid |
Second stage – SR-119 | |
Powered by | 1 Solid |
Maximum thrust | 1,365 kilonewtons (307,000 lbf) |
Burn time | 54 seconds |
Propellant | Solid |
Third stage – SR-120 | |
Powered by | 1 Solid |
Maximum thrust | 329 kilonewtons (74,000 lbf) |
Burn time | 62 seconds |
Propellant | Solid |
Fourth stage – Star-48V | |
Powered by | 1 Solid |
Maximum thrust | 64 kilonewtons (14,000 lbf) |
Burn time | 84 seconds |
Propellant | Solid |
Fifth stage (Baseline) – Star-37FM | |
Powered by | 1 Solid |
Maximum thrust | 47.26 kilonewtons (10,620 lbf) |
Burn time | 63 seconds |
Propellant | Solid |
Fifth stage (Optional) – Star-37FMV | |
Powered by | 1 Solid |
Propellant | Solid |
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.[1]
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.[2] 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.[2] 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[update], no launches are scheduled from anywhere except at MARS.[3]
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}}
- ^ "Lunar Atmosphere and Dust Environment Explorer (LADEE) Mission website". NASA.
- ^ a b "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.