Heavy-lift launch vehicle
A heavy-lift launch vehicle, or HLV or HLLV, is an orbital launch vehicle capable of lifting between 20,000 to 50,000 kg to low Earth orbit.[1] Operational heavy-lift launch vehicles included the Ariane 5, the Proton-M, the Delta IV Heavy, and the Long March 5.[2]
Heavy-lift rated launch vehicles
Rocket | In service | Manufacturer | Max. LEO payload | Heaviest launch | |
---|---|---|---|---|---|
…to LEO | …to GTO | ||||
OperationalThose currently operational rockets have demonstrated heavy-lift capability to low Earth orbit. | |||||
Ariane 5 ECA and ES | since 2002 | Airbus for ESA | 21,000 kg (46,000 lb)[3] | 20,293 kg (44,738 lb)[4] Georges Lemaître ATV July 29, 2014 |
10,865 kg (23,953 lb)[5] ViaSat-2 and Eutelsat 172B June 1, 2017 |
Delta IV Heavy[lower-alpha 1] | since 2004 | ULA | 28,790 kg (63,470 lb)[6] | Actual payloads flown are classified under the NRO launch program. | |
Proton-M | since 2001[lower-alpha 2] | Khrunichev | 23,000 kg (51,000 lb)[7] | 22,776 kg (50,212 lb)[8] Zvezda[lower-alpha 3] July 12, 2000 |
6,740 kg (14,860 lb)[9] ViaSat-1 October 19, 2011 |
UnprovenThe following rockets have not yet flown with a 20-tonne payload to LEO that would qualify them as an HLLV. | |||||
Angara A5 | since 2014 | Khrunichev | 24,500 kg (54,000 lb)[10] | N/A | 2,000 kg (4,400 lb)[11] Mass simulator December 23, 2014 |
Falcon 9 Full Thrust | since 2015 | SpaceX | 22,800 kg (50,300 lb)[12] (expendable version)[lower-alpha 4] |
9,600 kg (21,200 lb)[13] Iridium NEXT × 10 January 14, 2017 |
6,070 kg (13,380 lb)[14] Inmarsat-5 F4 May 15, 2017 |
Long March 5 (CZ-5) | since 2016 | CALT | 25,000 kg (55,000 lb)[15] | N/A | 4,000 kg (8,800 lb)[16] Shijian 17 November 3, 2016 |
- ↑ Delta IV Heavy is the world's highest capacity rocket currently in operation.
- ↑ Prior version Proton-K has flown operationally from 1970 to 2012.
- ↑ Zvezda was launched by a Proton-K version; Proton-M is slightly more powerful.
- ↑ The Falcon 9 reusable configuration only fits the medium-lift launch vehicle criteria.
Former HLLVs
The following HLLVs were formerly operational:
- Saturn IB, 1966 to 1975 (retired after 9 launches) Chrysler (S-IB), Douglas (S-IVB) Payload to LEO: 21,000 kg (46,000 lb) [17]
- Saturn V, 1967 to 1973 (retired after 13 launches) Payload to LEO:130,000 kg (290,000 lb) </ref>https://www.space.com/18422-apollo-saturn-v-moon-rocket-nasa-infographic.html.
- Proton-K 1967 to 2012 (retired after 311 launches) - Khrunichev State Research and Production Space Center Payload to LEO: 19,760 kg (43,560 lb) (nominal), 22,776 kg (50,212 lb) (demonstrated with Zvezda) [18]
- Space Shuttle, 1981 to 2011 (retired after 135 launches) United Space Alliance, Thiokol/Alliant Techsystems (SRBs), Lockheed Martin/Martin Marietta (ET), Boeing/Rockwell (orbiter) Payload to LEO: 24,400 kg (53,800 lb) (cargo bay payload only) [19]
- Titan IV, 1989 to 2005 (retired after 39 launches) - Lockheed Martin Payload to LEO: 21,680 kg (47,800 lb) [20]
In development
Four HLLVs are currently being developed:
- Ariane 6 - European Space Agency Payload to LEO: Unknown[lower-alpha 1] [21]
- Falcon Heavy in a partially reusable configuration[lower-alpha 2] - SpaceX Payload to LEO: 32,640 kg (71,960 lb)-38,080 kg (83,950 lb) (estimated)[22]
- New Glenn - Blue Origin Payload to LEO: 35,000 kg (77,000 lb)-70,000 kg (150,000 lb)[lower-alpha 3] (estimated) [23]
- Vulcan - United Launch Alliance Payload to LEO: 36,000 kg (79,000 lb) (estimated) [24][25]
- ↑ Payload to LEO presumed to be similar to Ariane 5 ES or ECA
- ↑ A fully expendable configuration is classified as a super heavy-lift launch vehicle since payload to LEO is over 50,000 kg
- ↑ If the upper part of this estimated payload range (>50,000 kg to LEO) is more accurate, then classification is as a super heavy-lift launch vehicle
Earlier concepts
- (NASA's Ares I was in the planning stages when canceled in 2010)[26] Payload to LEO: 25,400 kg (56,000 lb)
See also
- Sounding rocket, suborbital launch vehicle
- Small-lift launch vehicle, capable of lifting up to 2,000 kg to low Earth orbit
- Medium-lift launch vehicle, capable of lifting between 2,000 and 20,000 kg (4,400 to 44,100 lb) of payload into Low Earth orbit
- Super heavy-lift launch vehicle, capable of lifting more than 50,000 kg (110,000 lb) of payload into Low Earth orbit
- Comparison of orbital launch systems
- Comparison of orbital rocket engines
- Comparison of space station cargo vehicles
- Rocket
- Spacecraft propulsion
References
- ↑ NASA Space Technology Roadmaps - Launch Propulsion Systems, p.11: "Small: 0-2t payloads, Medium: 2-20t payloads, Heavy: 20-50t payloads, Super Heavy: >50t payloads"
- ↑ May, Sandra (August 27, 2014). "What Is a Heavy Lift Launch Vehicle?". NASA. Retrieved June 11, 2017.
- ↑ "Ariane 5 Users Manual, Issue 4, P. 39 (ISS orbit)" (PDF). Arianespace. Archived from the original (PDF) on 2007-09-27. Retrieved 2007-11-13.
- ↑ "Lanzamiento del ATV-5 Georges Lemaître (Ariane 5 ES)".
- ↑ "Arianespace marks its 2017 mid-year launch milestone with a record-setting Ariane 5 mission at the service of ViaSat and Eutelsat" (Press release). Arianespace. 1 June 2017. Retrieved 2 June 2017.
- ↑ Delta IV Launch Services User’s Guide, June 2013
- ↑ "Proton Launch System Mission Planner's Guide – Section 2. LV Performance" (PDF). International Launch Services. July 2009. Retrieved June 11, 2017.
- ↑ "Zvezda Service Module". Khrunichev. Retrieved June 11, 2017.
- ↑ Krebs, Gunter. "ViaSat 1". Gunter's Space Page. Retrieved June 11, 2017.
- ↑ Spaceflight101, Angara-a5
- ↑ "Russia made its first test launch "Angara-A5"". RIA Novosti. December 23, 2014. Retrieved December 23, 2014.
- ↑ Capabilities & Services (2016)
- ↑ de Selding, Peter B. (June 15, 2016). "Iridium's SpaceX launch slowed by Vandenberg bottleneck". SpaceNews. Retrieved June 11, 2017.
Each Iridium Next satellite will weigh 860 kilograms at launch, for a total satellite payload mass of 8,600 kilograms, plus the 1,000-kilogram dispenser.
- ↑ Graham, William (May 15, 2017). "SpaceX Falcon 9 in flawless Inmarsat-5 F4 launch". NASASpaceFlight.com. Retrieved June 11, 2017.
- ↑ Space launch report, CZ-5-7 Data Sheet
- ↑ Krebs, Gunter. "SJ 17". Gunter's Space Page. Retrieved June 11, 2017.
- ↑ Entering the Race to the Moon, Saturn IB Established Its Place in Space.
- ↑ http://www.khrunichev.ru/main.php?id=54
- ↑ astronautix.com, Space Shuttle
- ↑ astronautix.com, Titan IV
- ↑ "Ariane 6 design finalized, set for 2020 launch". Space Daily. 28 January 2016. Retrieved 30 January 2016.
- ↑ https://twitter.com/elonmusk/status/726559990480150528
- ↑ Berger, Eric (13 September 2016). "Falcon Heavy? New Glenn? NASA chief says he’s not a "big fan"". Ars Technica. Retrieved 8 December 2016.
- ↑ http://www.spacelaunchreport.com/vulcan.html
- ↑ Space Flight Now, ULA unveils its future with the Vulcan rocket family, April 13, 2015, by Justin Ray
- ↑ "Constellation Is Dead, But Pieces Live On". Aviation Week, October 26, 2010.
Further reading
- Mallove, Eugene F. and Matloff, Gregory L. The Starflight Handbook: A Pioneer's Guide to Interstellar Travel, Wiley. ISBN 0-471-61912-4.
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