Comparison of orbital launch systems
This is the comparison of orbital launch systems page. It contains two lists of conventional orbital launch systems (individual rocket configurations), separated by operational status. For the simple list of all conventional launcher families, see: Comparison of orbital launchers families. For the list of predominantly solid-fueled orbital launch systems, see: Comparison of solid-fueled orbital launch systems.
Spacecraft propulsion[note 1] is any method used to accelerate spacecraft and artificial satellites. A conventional solid rocket or a conventional solid-fuel rocket is a rocket with a motor that uses solid propellants (fuel/oxidizer).[note 2] Orbital launch systems are rockets and other systems capable of placing payloads into or beyond Earth orbit. All current spacecraft use conventional chemical rockets (bipropellant or solid-fuel) for launch, though some[note 3] have used air-breathing engines on their first stage.[note 4]
Current and upcoming rockets
Orbits legend:
- LEO, low Earth orbit
- SSO or SSPO, near-polar Sun-synchronous orbit
- polar, polar orbit
- MEO, medium Earth orbit
- GTO, geostationary transfer orbit
- GEO, geostationary orbit (direct injection)
- HEO, high Earth orbit
- HCO, heliocentric orbit
- TLI, trans-lunar injection
- TMI, trans-Mars injection
- Launch system status legend
- Under developmentOperational
Vehicle | Origin | Manufacturer | Payload mass to ... (kg) | Orbital launches incl. failures[lower-alpha 1] | Date of flight | |||
---|---|---|---|---|---|---|---|---|
LEO | GTO | Other | First[lower-alpha 2] | Latest | ||||
Alpha | Firefly Aerospace | 1,000[1] | 630 to SSO | 0 | 2020[2] | |||
Angara 1.2 | Khrunichev | 3,500[3] | 2,400 to SSO | 0 | 2020[4][lower-alpha 3] | |||
Angara A5 | Khrunichev | 24,000[3] | 7,500 with KVTK 5,400 with Briz-M [3] |
1 | 2014 | 2014 | ||
Antares 230 / 230+ | Northrop Grumman | 8,200[6] | 3,000 to SSO[lower-alpha 4] | 6[7] | 2016 | 2020 | ||
Ariane 5 ECA | EADS Astrium | 21,000[8] | 10,865[9][lower-alpha 5] | 73[11] | 2002 | 2019 | ||
Ariane 6 A62 | ArianeGroup | 10,350[12]:45 | 5,000[12]:33 | 6,450 to SSO 3,000 to HEO 3,000 to TLI [12]:40–49 |
0 | 2020[13][14] | ||
Ariane 6 A64 | ArianeGroup | 21,650[12]:46 | 11,500+ [12]:33 | 14,900 to SSO 5,000 to GEO 8,400 to HEO 8,500 to TLI [12]:40–49 |
0 | 2021–2022[13] | ||
Astra | Astra Space | 100[15] | 0 | 2020[15] | ||||
Atlas V 401 | ULA | 9,050[16] | 4,950 | 6,670 to SSO | 38[16] | 2002 | 2018 | |
Atlas V 411 | ULA | 9,050[16] | 6,075 | 8,495 to SSO | 5[16] | 2006 | 2018 | |
Atlas V 421 | ULA | 9,050[16] | 7,000 | 9,050 to SSO | 7[16] | 2007 | 2017 | |
Atlas V 431 | ULA | 9,050[16] | 7,800 | 9,050 to SSO | 3[16] | 2005 | 2016 | |
Atlas V 501 | ULA | 8,250[16] | 3,970 | 5,945 to SSO 1,500 to GEO |
6[16] | 2010 | 2020 | |
Atlas V 521 | ULA | 13,300[16] | 6,485 | 9,585 to SSO 2,760 to GEO |
2[16] | 2003 | 2004 | |
Atlas V 531 | ULA | 15,300[16] | 7,425 | 11,160 to SSO 3,250 to GEO |
3[16] | 2010 | 2013 | |
Atlas V 541 | ULA | 17,100[16] | 8,240 | 12,435 to SSO 3,730 to GEO |
6[16] | 2011 | 2018 | |
Atlas V 551 | ULA | 18,500[16] | 8,700 | 13,550 to SSO 3,960 to GEO |
10[16] | 2006 | 2019 | |
Atlas V N22[lower-alpha 6] | ULA | 13,000 | 1 | 2019[18] | ||||
Beta | Firefly Aerospace | 4,000[19] | TBA | 3,000 to SSO | 0 | TBA | ||
Bloostar | Zero 2 Infinity | 140[20] | 75 to SSO[20] | 0 | TBA | |||
Blue Whale 1 | Perigee Aerospace | 63[21] | 50 to SSO | 0 | 2020[22] | |||
Ceres-1 | Galactic Energy | 350 | 270 to SSO | 0 | 2020[23] | |||
Cyclone-4M | Yuzhnoye Yuzhmash |
5,000[24] | 1,000[25] | 3,350 to SSO[24] | 0 | 2021[26] | ||
Delta IV Heavy | ULA | 28,790[27] | 14,220 | 23,560 to polar 11,290 to TLI 8,000 to TMI |
11[28] | 2004 | 2019 | |
Electron | Rocket Lab | 225[29] | 150 to SSO | 12[30] | 2017 | 2020 | ||
Epsilon | IHI[31] | 1,500[32] | 590 to SSO | 4[33] | 2013 | 2019 | ||
Eris-S | Gilmour Space Technologies | 200[34] | 0 | 2021–2022[35] | ||||
Eris-L | Gilmour Space Technologies | 450[34] | 0 | TBA | ||||
Falcon 9 Full Thrust (partially reusable) |
SpaceX | 16,800+[36][lower-alpha 7] | 5,500[37][lower-alpha 8] | 9,600 to polar[39] | 55[40][41][lower-alpha 9] | 2015 | 2020 | |
Falcon 9 Full Thrust (expended) |
SpaceX | 22,800[37][lower-alpha 7] | 6,500[38]–8,300[37] | 4,020 to TMI | 14[44][45] | 2017 | 2020 | |
Falcon Heavy (partially reusable)[46] |
SpaceX | 30,000[47]–57,000[48] | 8,000[37]–10,000[lower-alpha 10] | 3[49][50] | 2018 | 2019 | ||
Falcon Heavy (expended) |
SpaceX | 63,800[37] | 15,000[38]–26,700[37] | 16,800 to TMI | 0 | – [lower-alpha 11] | ||
GSLV Mk II | ISRO | 5,000[51] | 2,700[52][lower-alpha 12] | 7[53] | 2010 | 2018 | ||
GSLV Mk III | ISRO | 10,000[54] | 4,000 | 4[55] | 2017[lower-alpha 13] | 2019 | ||
H-IIA 202 | Mitsubishi | 8,000[57]:67 | 4,000[57]:48 | 5,100 to SSO[lower-alpha 14] [57]:64–65 |
26[58] | 2001 | 2018 | |
H-IIA 204 | Mitsubishi | 5,950[57]:48 | 4[58] | 2006 | 2017 | |||
H3 | Mitsubishi | 4,000[59] | 6,500[60] | 4,000 to SSO[61] | 0 | 2020[61][62] | ||
Hyperbola-1 | i-Space | 300[63] | 1[64] | 2019[65][lower-alpha 15] | 2019 | |||
Hyperbola-2 | i-Space | 2,000[63] | 0 | 2021[63] | ||||
Jielong 1[66] | CALT | 200 (SSO) | 1[66] | 2019 | 2019 | |||
Kaituozhe-2 | CASC | 800[67] | 1[67] | 2017 | 2017 | |||
Kuaizhou 1/1A | ExPace | 400[68] | 9[68] | 2013[lower-alpha 16] | 2019 | |||
Kuaizhou 11 | ExPace | 1,500[69] | 1,000 to SSO[70] | 0 | 2020[71] | |||
Kuaizhou 21 | ExPace | 20,000[72] | 0 | 2025[70] | ||||
LauncherOne | Virgin Orbit | 500[73] | 300 to SSO[74] | 1 | 2020 | |||
Long March 2C | CALT | 3,850 |
1,250 with CTS2 | 2,000 to SSO with YZ-1S[75] | 57[76][lower-alpha 17] | 1982 | 2019 | |
Long March 2D | SAST | 4,000 | 1,150 to SSO | 46[76] | 1992 | 2020 | ||
Long March 2F | CALT | 8,600 | 13[76] | 1999 | 2016 | |||
Long March 3A | CALT | 6,000[77] | 2,600 | 5,000 to SSO | 27[78] | 1994 | 2018 | |
Long March 3B/E | CALT | 11,500[77] | 5,500 | 6,900 to SSO | 53[78] | 2007 | 2020 | |
Long March 3C | CALT | 9,100[77] | 3,800 | 6,500 to SSO | 17[78] | 2008 | 2019 | |
Long March 4B | SAST | 4,200[79] | 1,500 | 2,800 to SSO | 35[79] | 1999 | 2019 | |
Long March 4C | SAST | 4,200[80] | 1,500 | 2,800 to SSO | 28[79] | 2006 | 2019 | |
Long March 5 | CALT | 25,000[81] | 14,000 | 15,000 to SSO[82] 8,200 to TLI[83] 5,000 to TMI[83] |
3[82] | 2016 | 2019 | |
Long March 5B | CALT | 22,000[82] | 1[82] | 2020[84] | ||||
Long March 6 | SAST | 1,080 to SSO[85] | 3[86] | 2015 | 2019 | |||
Long March 7 | CALT | 13,500[87] | 5,500 to SSO | 2[88] | 2016[89] | 2017 | ||
Long March 7A | CALT | 5,500 to 7,000[84] | 1 | 2020 | 2020 | |||
Long March 8 (partially reusable)[90] |
CALT | 7,600[91] | 2,500 | 4,500 to SSO | 0 | 2021[90] | ||
Long March 9[92] | CALT | 140,000[93] | 66,000[94] | 50,000 to TLI[93] 44,000 to TMI[90] |
0 | 2028[95]–2030[90] | ||
Long March 11 | CALT | 700[96] | 350 to SSO | 8[97] | 2015 | 2019 | ||
Minotaur I | Northrop Grumman | 580[98] | 10[99] | 2000 | 2013 | |||
Minotaur IV | Northrop Grumman | 1,735[100] | 4[101] | 2010 | 2017 | |||
Minotaur V | Northrop Grumman | 670[101] | 465 to HCO | 1[101] | 2013 | 2013 | ||
Minotaur-C (Taurus)[102] | Northrop Grumman | 1,458[103] | 1,054 to SSO[lower-alpha 18] | 10[104] | 1994 | 2017 | ||
Miura 5 | PLD Space | 300[105] | 0 | 2021[105] | ||||
New Glenn | Blue Origin | 45,000[106] | 13,000 | 0 | 2021[107] | |||
New Line 1 (partially reusable)[108] |
LinkSpace | 200 to SSO[108] | 0 | 2020[108] | ||||
Nuri (KSLV-2) | KARI | 1,500 at 600–800 km[109] | 0 | 2021[109][lower-alpha 19] | ||||
OmegA Intermediate | Northrop Grumman | 22,000[110] | 9,200[110] | 3,200 to GEO[110] | 0 | 2021[111] | ||
OmegA Heavy | Northrop Grumman | 23,200[110] | 14,000[110] | 6,700 to GEO[110] | 0 | 2022[111] | ||
OS-M1 | OneSpace | 205[112] | 143 to SSO | 1 | 2019[113][lower-alpha 20] | 2019 | ||
OS-M2 | OneSpace | 390[112] | 292 to SSO | 0 | TBA | |||
Pegasus | Northrop Grumman | 500[115] | 44[115][116] | 1990 | 2019 | |||
Prime | Orbex | 220[117] | 150 to SSO[lower-alpha 4][118] | 0 | 2021[118] | |||
Proton-M / M+ | Khrunichev | 23,000 (M+)[119] 21,600 (M)[120] |
6,920 (M+) 6,150 (M) |
108[121][122][123] | 2001 | 2019 | ||
PSLV-CA | ISRO | 2,100[124] | 1,100 to SSO | 14[124] | 2007 | 2019 | ||
PSLV-DL | ISRO | 1[124] | 2019 | 2019 | ||||
PSLV-QL | ISRO | 2[124] | 2019 | 2019 | ||||
PSLV-XL | ISRO | 3,800[124] | 1,300 | 1,750 to SSO 1,350 to TMI[125] |
21[124] | 2008 | 2019 | |
Qased | Operator: Iranian Revolutionary Guard Corps | 1 | 2020 | 2020 | ||||
RS1 | ABL Space Systems | 1,200[126] | 400 | 875 to SSO | 0 | 2020 | ||
Safir | Iranian Space Agency | 65[127] | 7[127][lower-alpha 21] | 2008 | 2019 | |||
Shavit | IAI | 300[128] | 10[129] | 1988 | 2016 | |||
Simorgh | Iranian Space Agency | 350[130] | 2[130][lower-alpha 22] | 2017 | 2019 | |||
Soyuz-2.1a | TsSKB-Progress | 7,020 from Baikonur[131] | 33[132][133][134] | 2006[lower-alpha 23] | 2019 | |||
Soyuz-2.1b | TsSKB-Progress | 8,200 from Baikonur[131] | 2,400[135] | 32[133][136] | 2006 | 2019 | ||
Soyuz ST-A | TsSKB-Progress Arianespace |
7,800 from Kourou[137] | 2,810 with Fregat[138] | 6[133] | 2011 | 2018 | ||
Soyuz ST-B | TsSKB-Progress Arianespace |
9,000 from Kourou[139] | 3,250 with Fregat[138] | 4,400 to SSO[140] | 16[133] | 2011 | 2019 | |
Soyuz-2-1v | TsSKB-Progress | 2,800[141] | 1,400 to SSO | 5[141] | 2013 | 2019 | ||
Soyuz-5 / Irtysh | TsSKB-Progress RSC Energia |
18,000[142] | 2,500 to GEO | 0 | 2022[143][144] | |||
Space Launch System Block 1[lower-alpha 24] | NASA / Boeing (core) Northrop Grumman (SRBs) |
95,000[145] | 26,000 to TLI[145] | 0 | 2021[146] | |||
SLS Block 1B[lower-alpha 25] | NASA / Boeing Northrop Grumman |
105,000[147] | 37,000 to TLI[145] | 0 | 2024[148] | |||
SLS Block 2[lower-alpha 26] | NASA / Boeing Northrop Grumman |
130,000[149] | 45,000 to HCO[145] | 0 | late 2020s (TBD) | |||
SS-520 | IHI Aerospace | 4[150] | 2[151] | 2017[152][lower-alpha 27] | 2018 | |||
SSLV | ISRO | 500[153] | 300 to SSO | 0 | 2020[154] | |||
Starship[155] (Single launch) |
SpaceX | 100,000+[155][note 5] | 21,000[156] | 0 | 2020[157] | |||
Starship[155] (Additional refuelling launches) |
SpaceX | 100,000+[155][note 6] | 100,000+ [155] |
100,000+ to Mars surface[155] 100,000+ to lunar surface[155] |
0 | 2023[158] | ||
Terran 1 | Relativity Space | 1,250[159] | 900 to SSO | 0 | 2021[160] | |||
Unha | KCST | 100[161] | 4[162] | 2009[lower-alpha 28] | 2016 | |||
Vega | ESA / ASI | 1,500[lower-alpha 29][163] | 1,330 to SSO[164] | 15[165] | 2012 | 2019 | ||
Vega C | ESA / ASI | 2,200[lower-alpha 29][166] | 0 | 2020[167] | ||||
Vega E | ESA / ASI | 3,000[lower-alpha 29][168] | 0 | 2024[169] | ||||
Vikram l[170] | Skyroot aerospace[171] | 280 | 200 to SSPO | 0 | 2021[172] | |||
Vikram ll[170] | Skyroot aerospace | 520 | 410 to SSPO | 0 | TBA | |||
Vikram lll[170] | Skyroot aerospace | 720 | 580 to SSPO | 0 | TBA | |||
Vulcan / Centaur | ULA | 27,000[173] | 14,000[173] | 6,500 to GEO[173] 11,300 to TLI [12]:40–49 |
0 | 2021[174] | ||
Vulcan / ACES | ULA | 27,000[173] | 14,400[lower-alpha 30] | 7,200 to GEO [lower-alpha 30] 12,100 to TLI [173] |
0 | 2023[175] | ||
Yun Feng | National Chung-Shan Institute of Science and Technology | 200[176] | 0 | TBA | ||||
Yenisei[177] | TsSKB-Progress RSC Energia |
88,000 – 115,000[144] | 20,000 to TLI[178][179] | 0 | 2028[179] | |||
Zero | Interstellar Technologies | 100 to SSO[lower-alpha 4][180] | 0 | 2022–2023[181] | ||||
Zhuque-1 | LandSpace | 300[182] | 200 to SSO | 1[183] | 2018[183] | 2018 | ||
Zhuque-2 | LandSpace | 4,000[184] | 2,000 to SSO | 0 | 2020[185] |
- Suborbital flight tests and on-pad explosions are excluded, but launches failing en route to orbit are included.
- Effective year for active rockets, planned year for rockets in development
- A suborbital flight was conducted in 2014 as Angara-1.2pp, testing only the first and second stages.[5]
- Reference altitude 500 km
- Upgraded to 11,115 kg by 2020[10]
- for Starliner[17]
- PAF structural limit: 10,886 kg[43]
- GTO payload is 5,550 kg when the first stage lands downrange on a drone ship (ASDS). Reduced to 3,500 kg if the first stage returns to the launch site (RTLS).[38]
- Additionally, one rocket exploded on the launch pad in 2016.[42]
- GTO payload is 8,000 kg when the core first-stage booster lands downrange on a drone ship (ASDS) and the side boosters return to the launch site (RTLS). Increased to 10,000 kg if all boosters land on drone ships.[38]
- As of 2019 Falcon Heavy has only flown in partially reusable configuration; fully expendable configuration is considered operational in the sense that it is a simplified version of the reusable configuration.
- GTO payload with enhanced engines, as of GSLV version 2A[53]
- A suborbital test flight was conducted in 2014 (designated LVM-3/CARE) without the cryogenic upper stage (CUS).[56]
- 5,100 kg to a 500-km Sun-synchronous orbit; 3,300 kg to 800 km[57]:64–65
- A suborbital test flight was conducted in April 2018.[63]
- A suborbital test flight was conducted in March 2012.[68]
- Includes 6 possible launches of CZ-2C (3) noted by Gunter Krebs in reference [76].
- Reference altitude 400 km
- A suborbital test flight was conducted in November 2018.
- A suborbital test flight was conducted in May 2018.[114]
- Additionally, two rockets exploded on the launch pad, one in 2012 and one in 2019.[127]
- A suborbital test flight succeeded in 2016; both orbital flights in 2017 and 2019 failed.[130]
- Suborbital test flight in 2004, without Fregat upper stage.[132]
- with ICPS
- with EUS
- with EUS and
advanced boosters - A prior version of the SS-520 flew twice as a suborbital sounding rocket in 1998 and 2000. In 2017, the addition of a small third stage enabled orbital launches of ultra-light nano- or picosatellites.[150]
- A suborbital test flight failed in 2006. The first two orbital missions failed in 2009 and 2012, and the rocket finally reached orbit in late 2012.[162]
- Reference altitude 700 km
Retired and canceled rockets
- First suborbital test in 1969, first orbital launch attempt in 1970
- Without Buran, and assuming payload providing orbital insertion
- The U.S. Space Shuttle Transportation System and the Soviet Energia-Buran system consist of launch vehicle rockets and returnable spaceplane orbiter. Payload values listed here are for the mass of the payload in cargo bay of the spaceplanes, excluding the mass of the spaceplanes themselves.
- The SpaceX website lists the F9 payload to LEO as 13,150kg. The payload to GTO is listed as 4,850kg. However, SpaceX has stated that these numbers include a 30% margin to accommodate re-usability.
- Suborbital test flights in 1995, 1997 and 2002, no orbital launches attempted
- The N1 rocket was initially designed for 75mt LEO capacity and launch attempts were made with this version, but there were studies to increase the payload capacity to 90–95 mt, if a liquid-hydrogen upper stage engine could be developed.
- The Saturn V made 13 launches, 12 of which reached the correct orbits, and the other (Apollo 6) reached a different orbit than the one which had been planned; however, some mission objectives could still be completed; NASA, Saturn V News Reference, Appendix: Saturn V Flight History (1968) Archived 2011-05-17 at the Wayback Machine. For more information, see the Saturn V article. The Saturn V launch record is usually quoted as having never failed, e.g. "The rocket was masterminded by Wernher Von Braun and did not fail in any of its flights", Alan Lawrie and Robert Godwin; Saturn, but the Apollo 6 launch should be considered a partial mission failure. The 13th launch of Saturn V was in special configuration (SA-513) with the Skylab.
- A third rocket exploded before launch.
- First orbital launch attempt in 2005
Launch systems by country
The following chart shows the number of launch systems developed in each country, and broken down by operational status. Rocket variants are not distinguished; i.e., the Atlas V series is only counted once for all its configurations 401–431, 501–551, 552, and N22.
- Operational
- In development
- Retired
See also
- Comparison of orbital launchers families
- Comparison of orbital rocket engines
- Comparison of space station cargo vehicles
- List of space launch system designs
- List of orbital launch systems
- Lists of rockets
- List of sounding rockets
- List of upper stages
- Non-rocket spacelaunch
Notes
- There are many different methods. Each method has drawbacks and advantages, and spacecraft propulsion is an active area of research. However, most spacecraft today are propelled by forcing a gas from the back/rear of the vehicle at very high speed through a supersonic de Laval nozzle. This sort of engine is called a rocket engine.
- The first medieval rockets were solid-fuel rockets powered by gunpowder; they were used by the Chinese, Indians, Mongols and Arabs, in warfare as early as the 13th century.
- Such as the Pegasus rocket and SpaceShipOne.
- Most satellites have simple reliable chemical thrusters (often monopropellant rockets) or resistojet rockets for orbital station-keeping and some use momentum wheels for attitude control. Soviet bloc satellites have used electric propulsion for decades, and newer Western geo-orbiting spacecraft are starting to use them for north-south stationkeeping and orbit raising. Interplanetary vehicles mostly use chemical rockets as well, although a few have used ion thrusters and Hall effect thrusters (two different types of electric propulsion) to great success.
- Elon Musk [@elonmusk] (31 March 2020). "Mass of initial SN ships will be a little high & Isp a little low, but, over time, it will be ~150t to LEO fully reusable" (Tweet) – via Twitter.
- Elon Musk [@elonmusk] (31 March 2020). "Mass of initial SN ships will be a little high & Isp a little low, but, over time, it will be ~150t to LEO fully reusable" (Tweet) – via Twitter.
References
- "Firefly Alpha". Firefly Aerospace. Retrieved 29 October 2019.
- Clark, Steven (18 June 2019). "Firefly Offering Free Launch For Research and Education Payloads". SpaceFlightNow. Retrieved 19 June 2019.
- "Angara Launch Vehicle Family". Khrunichev State Research and Production Space Center. Retrieved 2 September 2018.
- SLP studio (17 October 2018). "Раскрыты планы пусков ракет "Протон" и "Ангара" на 2019 год" [2019 launch plans for Proton and Angara have been announced] (in Russian). Retrieved 25 October 2018 – via Yandex Zen.
- Graham, William (9 July 2014). "Angara rocket launches on maiden flight". NASASpaceFlight.com. Retrieved 2 September 2018.
- Krebs, Gunter. "Antares (Taurus-2)". Gunter's Space Page. Retrieved 1 December 2019.
- Krebs, Gunter. "Antares 230". Gunter's Space Page. Retrieved 20 November 2019.
- "Ariane 5 Users Manual" (PDF). Issue 4. Arianespace. p. 39 (ISS orbit). Archived from the original (PDF) on 27 September 2007. Retrieved 13 November 2007.
- Clark, Stephen (2 June 2017). "Ariane 5 succeeds in launch of two high-value communications satellites". Spaceflight Now. Retrieved 17 January 2018.
- "Arianespace begins building final 10 Ariane 5s ahead of Ariane 6 operational debut". Space Daily. 10 January 2018. Retrieved 17 January 2018.
Ariane 5 set a new record in June 2017 by lofting 10,865 kg. into geostationary transfer orbit (GTO). From this payload lift record, Ariane 5's performance will be increased another 250 kg.
- Krebs, Gunter. "Ariane-5". Gunter's Space Page. Retrieved 30 November 2019.
- Lagier, Roland (March 2018). "Ariane 6 User's Manual Issue 1 Revision 0" (PDF). Arianespace. Retrieved 27 May 2018.
- Clark, Stephen (13 August 2016). "Ariane 6 rocket holding to schedule for 2020 maiden flight". Spaceflight Now. Retrieved 13 August 2016.
- Krebs, Gunter. "Ariane-6". Gunter's Space Page. Retrieved 2 September 2018.
- Vance, Ashlee (3 February 2020). "A Small-Rocket Maker Is Running a Different Kind of Space Race". Bloomberg News. Retrieved 3 February 2020.
- Krebs, Gunter. "Atlas-5". Gunter's Space Page. Retrieved 10 August 2019.
- Egan, Barbara [@barbegan13] (October 15, 2016). "We are calling the config N22. No payload fairing with the Starliner on board" (Tweet) – via Twitter.
- Roulette, Joey (22 December 2019). "'Bull's-eye' landing in New Mexico for Boeing's Starliner astronaut capsule". Reuters. Retrieved 22 December 2019.
- "Firefly Beta". Firefly Aerospace. Archived from the original on 12 August 2018. Retrieved 11 August 2018.
- "Bloostar Launch Vehicle Payload User's Guide" (PDF). Revision 2. Zero 2 Infinity. January 2018. Z2I-BS-TN-1-0316-R2. Retrieved 4 September 2018.
- "Perigee Aerospace Inc". Retrieved 2020-06-14.
- "Korean firm Perigee plans first South Australian rocket launch". 28 October 2019.
- "Ceres-1". Gunter's Space page. Retrieved 2020-02-20.
- Boucher, Marc (14 March 2017). "Exclusive: Maritime Launch Services Selects Nova Scotia Site for Spaceport Over 13 Other Locations". SpaceQ. Retrieved 18 March 2017.
- Krebs, Gunter. "Tsiklon-4M (Cyclone-4M)". Gunter's Space Page. Retrieved 11 April 2017.
- "Cyclone 4M fully integrated upper stage performs successful qualification test" (Press release). Yuzhnoye Design Office and Maritime Launch Services. 21 October 2019. Retrieved 1 December 2019.
- "Delta IV Launch Services User's Guide, June 2013" (PDF). United Launch Alliance. June 2013. pp. 2–10. Retrieved 9 October 2017.
- Krebs, Gunter. "Delta-4". Gunter's Space Page. Retrieved 17 March 2019.
- "Electron". Rocket Lab. Retrieved 31 August 2018.
- "Completed Missions". Rocket Lab. Retrieved 2020-06-14.
- "Projects&Products". IHI Aerospace. Archived from the original on 6 April 2011. Retrieved 8 March 2011.
- "Epsilon a solid propellant launch vehicle for new age" (PDF). IHI Aerospace. Retrieved 3 February 2018.
- Krebs, Gunter. "Epsilon". Gunter's Space Page. Retrieved 18 January 2019.
- "ERIS-S | ERIS-L". Gilmour Space Technologies. Retrieved 1 December 2019.
- "Launching small satellites to LEO from 2021/22". Gilmour Space Technologies. Retrieved 1 December 2019.
- https://www.digitaltrends.com/cool-tech/spacex-launches-its-first-batch-of-starlink-internet-satellites/
- "Capabilities & Services". SpaceX. Retrieved 5 April 2017.
- Koenigsmann, Hans (3 October 2018). SpaceX performance tiers to GTO. IAC 2018. Retrieved 23 October 2018.
- de Selding, Peter B. (June 15, 2016). "Iridium's SpaceX launch slowed by Vandenberg bottleneck". SpaceNews. Retrieved June 21, 2016.
- Krebs, Gunter. "Falcon-9 v1.2 (Falcon-9FT)". Gunter's Space Page. Retrieved 19 November 2018.
- Krebs, Gunter. "Falcon-9 v1.2 (Block 5) (Falcon-9FT (Block 5))". Gunter's Space Page. Retrieved 20 November 2019.
- Malik, Tariq (1 September 2016). "Launchpad Explosion Destroys SpaceX Falcon 9 Rocket, Satellite in Florida". Space.com. Retrieved 1 September 2016.
- "Falcon 9 Launch Vehicle – Payload User's Guide" (PDF). Revision 2. SpaceX. 21 October 2015. p. 15. Archived from the original (PDF) on 14 March 2017. Retrieved 29 November 2015.
- Krebs, Gunter. "Falcon-9 v1.2(ex) (Falcon-9FT(ex))". Gunter's Space Page. Retrieved 29 June 2018.
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- Either 2 or 3 boosters recoverable
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