Minotaur V
The Minotaur V is an American expendable launch system derived from the Minotaur IV, itself a derivative of the LGM-118 Peacekeeper ICBM. It was developed by Orbital Sciences Corporation, (now absorbed into Northrop Grumman Innovation Systems) and made its maiden flight on 7 September 2013 carrying the Lunar Atmosphere and Dust Environment Explorer spacecraft for NASA.[2]
The first Minotaur V at MARS before the launch of LADEE. | |
| Function | Expendable launch system |
|---|---|
| Manufacturer | Northrop Grumman (Northrop Grumman Innovation Systems) |
| Country of origin | United States |
| Size | |
| Height | 24.56 m[1] |
| Diameter | 2.34 m[1] |
| Mass | 89,373 kg[1] |
| Stages | Five |
| Capacity | |
| Payload to GTO | |
| Mass | 532 kg |
| Payload to TLI | |
| Mass | 342 kg |
| Associated rockets | |
| Family | Minotaur |
| Launch history | |
| Status | Active |
| Launch sites | SLC-8, Vandenberg AFB LP-0B, MARS LP-1, Kodiak |
| Total launches | 1 |
| Success(es) | 1 |
| First flight | 7 September 2013 |
| First stage – SR-118 | |
| Powered by | 1 Solid |
| Maximum thrust | 2,200 kN (490,000 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-48BV | |
| 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 |
Design edit
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 342 kilograms (754 lb) on a trans-lunar trajectory.[3] 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.[3] The Star-37FMV upper stage is heavier, reducing payload capacity, but is more maneuverable.
Launch pads edit
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], all scheduled launches are from MARS.[4]
Launch history edit
The initial launch of a Minotaur V occurred on 7 September 2013 at 03:27 UTC from Launch Pad 0B at the Mid-Atlantic Regional Spaceport in Virginia. The payload for the maiden flight was the LADEE lunar exoatmosphere science spacecraft.[5] While now separated from the LADEE spacecraft, both the fourth and fifth stages of the Minotaur V reached orbit, and are now derelict satellites in Earth orbit.[6]
References edit
- ^ a b c "Lunar Atmosphere and Dust Environment Explorer (LADEE) Launch" (PDF). NASA. Retrieved 8 September 2013.
- ^ . NASA. Archived from the original on 2010-03-29.
- ^ a b (PDF). Minotaur V. Orbital Sciences Corporation. Archived from the original (PDF) on 2006-03-11. Retrieved 22 January 2013.
- ^ Krebs, Gunter. "Minotaur-3/-4/-5 (OSP-2 Peacekeeper SLV)". Gunter's Space Page. Retrieved 22 January 2013.
- ^ Stephen Clark (7 September 2013). "Moon mission hits snag after flawless late-night launch". Spaceflight Now. Retrieved 7 September 2013.
- ^ Graham, William (6 September 2013). "Orbital's Minotaur V launches LADEE mission to the Moon". NASAspaceflight.com. Retrieved 8 September 2013.