Spaceflight before 1951
National firsts | |
---|---|
Spaceflight | Germany (1944) United States (1946) Soviet Union (1948) |
Rockets | |
Maiden flights | V-2 Viking (first model) Bumper Aerobee RTV-N-8 Aerobee RTV-N-10 Aerobee XASR-SC-1 Aerobee XASR-SC-2 Aerobee RTV-A-1 R-1 R-1A R-2E R-2 |
Retirements | Aerobee RTV-N-8 Bumper R-1A R-2E |
Spaceflight as a practical endeavor began during World War II with the development of operational liquid-fueled rockets. Beginning life as a weapon, the V-2 was pressed into peaceful service after the war at the United States' White Sands Missile Range as well as the Soviet Union's Kapustin Yar. This led to a flourishing of missile designs setting the stage for the exploration of space. The small American WAC Corporal rocket was evolved into the Aerobee, a much more powerful sounding rocket. Exploration of space began in earnest in 1947 with the flight of the first Aerobee, 46 of which had flown by the end of 1950. These and other rockets, both Soviet and American, returned the first direct data on air density, temperature, charged particles and magnetic fields in the Earth's upper atmosphere.
By 1948, the United States Navy had evolved the V-2 design into the Viking capable of more than 100 miles (160 km) in altitude. The first Viking to accomplish this feat, number four, did so 10 May 1950. The Soviet Union developed a virtual copy of the V-2 called the R-1, which first flew in 1948. Its longer-ranged successor, the R-2, entered military service in 1950. This event marked the entry of both superpowers into the post-V-2 rocketry era.
Origins and rocket development
The era of spaceflight began in 1942 with the development of the V-2 rocket (A-4) as a ballistic missile by Germany, the first vehicle capable of reaching the 100 kilometres (62 mi) boundary of space (as defined by the World Air Sports Federation).[1] On 20 June 1944, a V-2 (MW 18014) was launched vertically, reaching a height of 174.6 kilometres (108.5 mi).[2]
The post-war years saw rapid development in rocket technology by both superpowers, jumpstarted by the dozens of V-2s and hundreds of German specialists that ended up in the custody of the Soviet Union and the United States.[3]: 216–7 [4]: 226 [5]: 43 The V-2, designed for carrying a warhead horizontally rather than vertical science missions, made an inefficient sounding rocket, while the wartime American WAC Corporal sounding rocket was too small to carry much scientific equipment.[4]: 250 In 1946, the US Navy began development of its own heavy sounding rocket, the Viking, derived in part from the V-2.[6]: 21–25 [6]: 236 The Aerobee was developed from the WAC Corporal to loft lighter payloads.[4]: 250–1
The Soviet Union began military development of the R-1, a copy of the V-2 with modifications intended to improve reliability, in 1947.[5]: 41, 48 Flight testing of this first Soviet-made liquid-fueled missile began on 13 September 1948,[5]: 129 and the rocket entered military service in 1950.[5]: 135 Also from 1947, two advanced rockets with ranges of 600 kilometres (370 mi), the German émigré-designed G-1 (or R-10) and the Russian-designed R-2, competed for limited engineering and production staff, the latter winning out by the end of 1949[5]: 65 and being put into service in 1951.[5]: 274 The draft plan for the 3,000 kilometres (1,900 mi) range R-3 was approved on 7 December 1949,[5]: 67 though it was never developed, later designs proving more useful and achievable.[5]: 275–6
Space exploration
V-2, WAC Corporal, and R-1A
The V-2s captured from Germany at the end of World War II were used for engineering and scientific missions by the United States and the Soviet Union. The first 25 captured V-2s were launched in the 15 months commencing 15 March 1946.[4]: 398 By the end of 1950, more than 60 had been launched by the Americans, most of them equipped with research instruments.[7]: 6 The first biological payloads launched to high altitude were sent on V-2s, starting with seeds and fruit flies in 1947, followed by mice and monkeys from 1948 onward.[8]
The V-2 was also used in early experiments with two-stage rockets: Project Bumper combined the V-2 first stage with the WAC Corporal as second stage. On 24 February 1949, Bumper 5 set an altitude record of 417 kilometres (259 mi).[4]: 257–8 Around 10 WAC Corporals were also launched on their own in this period.[7]: 6
The Soviet Union launched 11 captured V-2s in 1947.[5]: 41 Three of the V-2s launched by the USSR in 1947 carried 500 kilograms (1,100 lb) experiment packages for measuring cosmic rays at high altitude; at least one returned usable data.[9]: 56 Two Soviet R-1As (an experimental R-1 variant that tested nose cone separation at altitude) also carried scientific equipment during test launches in 1949, but neither returned usable data.[10]
Aerobee
First launched on 24 November 1947, the solid/liquid-fuel hybrid Aerobee quickly secured a reputation for reliability. With the development of these first generation purpose-built sounding rockets, the exploration of Earth's upper atmosphere and the nearest reaches of space began in earnest, a total of 46 Aerobee flights being launched through 1950.[11] Aerobee flights measured the velocity and density of cosmic rays above 70 miles (110 km) and made high altitude measurements of the Earth's magnetic field. Cameras mounted on Aerobee rockets returned the first high quality aerial photographs of sizeable regions of the Earth as well as large scale cloud formations.[4]: 251
Viking
Vikings 1 and 2, launched in 1949 from White Sands Missile Range in New Mexico, both suffered from premature engine cutoff due to turbine leaks, significantly reducing their maximum altitude.[6]: 98–102 The improved Viking 3, launched 9 February 1950 reached 50 mi (80 km) and could have gone higher. However, after 34 seconds of accurately guided flight, the rocket veered westward and had to be destroyed by range safety.[6]: 108–114
On 10 May 1950, Viking 4 was launched from a site in the Pacific Ocean between Jarvis Island and Christmas Island. The fourth Viking became the first sounding rocket ever launched from a sea-going vessel, the USS Norton Sound. This flight was perfect, reaching 106.4 mi (171.2 km), more than double that reached by the earlier Vikings.[6]: 108–114
Viking 5, launched 21 November 1950, carried a vast array of radiation detectors. The rocket also carried two movie cameras to take high altitude film of the Earth all the way to its peak height of 108 miles (174 km) as well as Pirani gauges to measure air densities in the upper atmosphere.[6]: 148, 236 Viking 6, launched 11 December, underperformed, reaching a maximum altitude of 40 miles (64 km).[6]: 151–153, 236
Launches
1942
Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
---|---|---|---|---|---|---|---|
Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
Remarks | |||||||
13 June — 12 December | V-2 | Peenemünde | Wehrmacht | ||||
Wehrmacht | Suborbital | Missile test | Same day | Mixed | |||
7 V-2 rockets launched on test flights, 3 successfully[12] |
1943
Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
---|---|---|---|---|---|---|---|
Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
Remarks | |||||||
7 Januaro — 30 December | V-2 | Peenemünde, Heidelager | Wehrmacht | ||||
Wehrmacht | Suborbital | Missile test | Same day | Mixed | |||
39 V-2 rockets launched on test flights; at least 9 failures[12] |
1944
Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
---|---|---|---|---|---|---|---|
Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
Remarks | |||||||
20 June | V-2 | Greifswalder Oie | Wehrmacht | ||||
MW 18014[2] | Wehrmacht | Suborbital | Missile test | 20 June | Successful | ||
First artificial object to cross the Kármán line. Vertical test, apogee: 174.6 kilometres (108.5 mi) | |||||||
8 September | V-2 | Houffalize | Wehrmacht | ||||
Wehrmacht | Suborbital | Missile attack | 8 September | Successful | |||
First combat usage of V-2 after more than a hundred test flights; ~3000 combat launches followed[12] (see List of V-2 test launches) |
1945
Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
---|---|---|---|---|---|---|---|
Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
Remarks | |||||||
2 October 13:41 |
V-2 | Cuxhaven | UK military | ||||
Suborbital | 2 October | Successful | |||||
First launch of Operation Backfire; apogee: 69.4 kilometres (43.1 mi)[13] | |||||||
4 October 13:15 |
V-2 | Cuxhaven | UK military | ||||
Suborbital | 4 October | Partial failure | |||||
Apogee: 17.4 kilometres (10.8 mi) [13] | |||||||
15 October 14:06 |
V-2 | Cuxhaven | UK military | ||||
Suborbital | 15 October | Successful | |||||
Press and international observers present; Apogee: 64 kilometres (40 mi)[13] |
1946
Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
---|---|---|---|---|---|---|---|
Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
Remarks | |||||||
16 April 21:47 |
V-2 | White Sands LC-33 | General Electric / US Army | ||||
WSPG[14] | Suborbital | Cosmic Radiation (Applied Physics Laboratory)[15] | 16 April | Guidance failure[14] | |||
First launch of Project Hermes, apogee: 8 kilometres (5.0 mi) | |||||||
10 May 21:15 |
V-2 | White Sands LC-33 | GE / US Army | ||||
WSPG[14] | Suborbital | Cosmic Radiation (APL)[15] | 10 May | Successful | |||
Project Hermes launch, apogee: 112 kilometres (70 mi), First US spaceflight | |||||||
29 May 21:12 |
V-2 | White Sands LC-33 | GE / US Army | ||||
GE[14] | Suborbital | Cosmic Radiation (APL)[15] | 29 May | Successful | |||
Project Hermes launch, apogee: 112 kilometres (70 mi) | |||||||
13 June 23:40 |
V-2 | White Sands LC-33 | GE / US Army | ||||
GE[14] | Suborbital | Solar radiation, Ionosphere (NRL)[15] | 13 June | Successful | |||
Project Hermes launch, apogee: 117 kilometres (73 mi) | |||||||
28 June 19:25 |
V-2 | White Sands LC-33 | GE / US Army | ||||
Naval Research Laboratory[14] | Suborbital | Cosmic Radiation, Solar Radiation, Pressure, Temperature. Ionosphere[16]: 336–337 (V-2 NO. 6) | 28 June | Successful | |||
Project Hermes launch, apogee: 108 kilometres (67 mi) | |||||||
9 July 19:25 |
V-2 | White Sands LC-33 | GE / US Army | ||||
GE[14] | Suborbital | Cosmic Radiation, Ionosphere (NRL), Biological (Harvard University)[16]: 338–339 (V-2 NO. 7) | 9 July | Successful | |||
Project Hermes launch, apogee: 134 kilometres (83 mi) | |||||||
19 July 19:11 |
V-2 | White Sands LC-33 | GE / US Army | ||||
GE[14] | Suborbital | Ionospheric (NRL)[15] | 19 July | Launch failure, explosion at 28.5 seconds[14] | |||
Project Hermes launch, apogee: 5 kilometres (3.1 mi) | |||||||
30 July 19:36 |
V-2 | White Sands LC-33 | GE / US Army | ||||
Applied Physics Laboratory[14] | Suborbital | Cosmic Radiation, Ionosphere (NRL)[16]: 342–343 (V-2 NO. 9) | 30 July | Successful | |||
Project Hermes launch, apogee: 167 kilometres (104 mi) | |||||||
15 August 18:00 |
V-2 | White Sands LC-33 | GE / US Army | ||||
Princeton University[14] | Suborbital | Cosmic Radiation, Ionosphere[16]: 344 (V-2 NO. 10) | 15 August | Guidance Failure at 13.9 seconds[14] | |||
Project Hermes launch, apogee: 3 kilometres (1.9 mi) | |||||||
22 August 17:15 |
V-2 | White Sands LC-33 | GE / US Army | ||||
University of Michigan[14] | Suborbital | Pressure, Density, Ionosphere Aeronomy, Sky Brightness[15] | 22 August | Guidance Failure immediately after lift[14] | |||
Project Hermes launch | |||||||
10 October 18:02 |
V-2 | White Sands LC-33 | GE / US Army | ||||
NRL[14] | Suborbital | Cosmic Ray, Ionosphere, Pressure-Temperature, Solar Spectroscopy, Ejection of Cosmic Ray Recording Camera[17] Selected seeds (Harvard), Cross jet attenuation transmitter & receiver[16]: 346–347 (V-2 NO. 12) | 10 October | Successful | |||
Project Hermes launch, apogee: 164 kilometres (102 mi) | |||||||
24 October 19:15 |
V-2 | White Sands LC-33 | GE / US Army | ||||
APL[14] | Suborbital | Cosmic & Solar radiation, winds, photography[15] | 24 October | Successful, Short burning time (59 sec)[18] | |||
Project Hermes launch, apogee: 105 kilometres (65 mi), First photo of Earth from space | |||||||
7 November 20:31 |
V-2 | White Sands LC-33 | GE / US Army | ||||
Princeton University[14] | Suborbital | Cosmic Radiation[15] | 7 November | Guidance Failure at 2 seconds, missile turned sideways, flew horizontal and was destroyed[16]: 350 (V-2 NO. 14) | |||
Project Hermes launch, apogee: 0.39 kilometres (0.24 mi) | |||||||
21 November 16:55 |
V-2 | White Sands LC-33 | GE / US Army | ||||
Watson Laboratories, University of Michigan[18] | Suborbital | Pressure, Temperature, Ionosphere, Sky Brightness, Voltage breakdown[16]: 351–352 (V-2 NO. 15) | 21 November | Successful | |||
Project Hermes launch, apogee: 102 kilometres (63 mi) | |||||||
5 December 20:08 |
V-2 | White Sands LC-33 | GE / US Army | ||||
NRL[14] | Suborbital | Cosmic & Solar Radiation, Pressure, Temperature, Photography[15] | 5 December | Successful, Guidance Problems | |||
Project Hermes launch, apogee: 167 kilometres (104 mi) | |||||||
18 December 05:12 |
V-2 | White Sands LC-33 | GE / US Army | ||||
GRENADES | APL[14] | Suborbital | Cosmic Radiation, Meteor research, Biological (National Institute of Health)[15] | 18 December | Successful, extraordinary range due to guidance failure[16]: 354 (V-2 NO. 16) | ||
Project Hermes launch, apogee: 187 kilometres (116 mi); first night flight of V-2, released artificial meteors for photographic observation[19] |
1947
Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
---|---|---|---|---|---|---|---|
Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
Remarks | |||||||
10 January 21:13 |
V-2 | White Sands LC-33 | GE / US Army | ||||
NRL[14] | Suborbital | Cosmic Radiation,[15] "Daughter" Canister Release (Air Material Command)[16]: 357–358 (V-2 NO. 18) | 10 January | Successful, Roll at 40 seconds[14] | |||
Project Hermes launch, apogee: 116 kilometres (72 mi) | |||||||
24 January 00:22 |
V-2 | White Sands LC-33 | GE / US Army | ||||
GE[14] | Suborbital | Test Guidance System,[14] Hermes A-2 Telemetry System Test[16]: 359–360 (V-2 NO. 19) | 24 January | Successful | |||
Project Hermes launch, apogee: 49.88 kilometres (30.99 mi). | |||||||
20 February 18:16 |
V-2 | White Sands LC-33 | GE / US Army | ||||
Blossom I | Air Materiel Command[14] | Suborbital | Pressure-temperature (University of Michigan), Ionosphere (Air Force Cambridge Research Center, UoM), Sky brightness, Voltage Breakdown measurements (AFCRC), Biological rye, cotton seeds and fruit flies, first animals in space,[20] Blossom parachute recovery of canister (Cambridge Field Station)[16]: 361–362 (V-2 NO. 20) | 20 February | Successful, Guidance disturbance at 27 sec, Roll at 37.5 sec[14] | ||
Project Hermes launch, apogee: 109 kilometres (68 mi). | |||||||
7 March 18:23 |
V-2 | White Sands LC-33 | GE / US Army | ||||
NRL[14] | Suborbital | Cosmic Radiation, Pressure-temperature, Solar Radiation, Ionosphere (NRL), Biological rye, cotton seeds and fruit flies (Harvard)[16]: 363–365 (V-2 NO. 21) | 7 March | Successful | |||
Project Hermes launch, apogee: 161 kilometres (100 mi). | |||||||
1 April 20:10 |
V-2 | White Sands LC-33 | GE / US Army | ||||
APL[14] | Suborbital | Cosmic Radiation, Solar Radiation (APL & Yerkes Observatory), High altitude photography (Gun Sight Aiming Point camera)[16]: 366–367 (V-2 NO. 22) | 1 April | Successful | |||
Project Hermes launch, apogee: 129 kilometres (80 mi) | |||||||
9 April 00:10 |
V-2 | White Sands LC-33 | GE / US Army | ||||
APL[14] | Suborbital | Cosmic Radiation, Solar Radiation, High altitude photography.[16]: 368–369 (V-23 NO. 20) | 9 April | Successful | |||
Project Hermes launch, apogee: 103 kilometres (64 mi) | |||||||
17 April 23:22 |
V-2 | White Sands LC-33 | GE / US Army | ||||
GRENADES | GE[14] | Suborbital | Pressure-Temperature: 9 Grenades (Signal Corps Engineering Laboratories)[16]: 370–371 (V-2 NO. 24) | 17 April | Successful, Roll at 57.5 seconds[14] | ||
Project Hermes launch, apogee: 140 kilometres (87 mi) | |||||||
15 May 23:08 |
V-2 | White Sands LC-33 | GE / US Army | ||||
NRL[14] | Suborbital | Density-pressure-temperature grenades (SCEL), (Michigan University), Composition, Cosmic Radiation, Solar Radiation (NRL)[16]: 374–375 (V-2 NO. 26) | 15 May | Successful, Steering trouble from lift[14] | |||
Project Hermes launch, apogee: 122 kilometres (76 mi) | |||||||
29 May | V-2 | White Sands LC-33 | GE / US Army | ||||
Hermes II | GE | Suborbital | Missile test of ramjet diffusers called "Organ"[21] | 29 May | Launch Failure, missile went South instead of North, landed in Mexico[22] | ||
Project Hermes launch, apogee: 50 kilometres (31 mi), maiden flight of Hermes II | |||||||
10 July 19:18 |
V-2 | White Sands LC-33 | GE / US Army | ||||
NRL[14] | Suborbital | Density-pressure-temperature, Cosmic Radiation, Ionosphere, Simulant agent experiment – Camp Detrick, Indiana, seed containers in control chamber (Harvard College Observatory)[16]: 363–364 (V-2 NO. 29) | 10 July | Launch failure, Steering trouble from lift[14] | |||
Project Hermes launch, apogee: 16 kilometres (9.9 mi) | |||||||
29 July 12:55 |
V-2 | White Sands LC-33 | GE / US Army | ||||
APL[14] | Suborbital | Cosmic Radiation, Solar Radiation, High altitude photography (APL)[16]: 386–387 (V-2 NO. 30) | 29 July | Successful, Vane #4 ceased to operate at 27 sec[14] | |||
Project Hermes launch, apogee: 159 kilometres (99 mi) | |||||||
6 September | V-2 | USS Midway, Atlantic Ocean Launch Site 10 | US Navy | ||||
US Navy | Suborbital | Missile test | 6 September | Launch failure | |||
Operation Sandy, first shipboard missile launch, apogee: 1 kilometre (0.62 mi) | |||||||
9 October 19:15 |
V-2 | White Sands LC-33 | GE / US Army | ||||
GE[14] | Suborbital | Density-pressure-temperature, Skin temperature, Composition (University of Michigan), Solar radiation (NRL)[16]: (V-2 NO. 27) | 9 October | Successful, Steering disturbance at 48.4 sec. Roll at 52 sec.[14] | |||
Project Hermes launch, apogee: 156 kilometres (97 mi) | |||||||
18 October 07:47 |
V-2 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 28 October | Partial failure | |||
Apogee: 86 kilometres (53 mi); destroyed during ballistic portion of flight[23] | |||||||
20 October 07:47 |
V-2 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 20 October | Partial failure | |||
Apogee: 85 kilometres (53 mi); tore loose from launch stand; flew 180 kilometres (110 mi) left of planned target[23] | |||||||
23 October 14:05 |
V-2 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 23 October | Launch failure | |||
Apogee: 14 kilometres (8.7 mi); payload destroyed, rocket disintegrated[23] | |||||||
28 October 14:05 |
V-2 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 28 October | Successful | |||
Apogee: 87 kilometres (54 mi)[23] | |||||||
31 October 13:41 |
V-2 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 31 October | Launch failure | |||
Apogee: 0 kilometres (0 mi); loss of control on longitudinal axis[23] | |||||||
2 November 15:14 |
V-2 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 2 November | Successful | |||
Apogee: 88 kilometres (55 mi)[23] | |||||||
3 November 12:05 |
V-2 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 3 November | Launch failure | |||
Apogee: 0 kilometres (0 mi); rolled after launch and lost stabilization[23] | |||||||
4 November 15:02 |
V-2 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 4 November | Successful | |||
Apogee: 89 kilometres (55 mi)[23] | |||||||
10 November 09:39 |
V-2 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 10 November | Launch failure | |||
Apogee: 11 kilometres (6.8 mi); lost guidance[23] | |||||||
13 November 08:30 |
V-2 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 13 November | Successful | |||
Apogee: 89 kilometres (55 mi)[23] | |||||||
13 November 14:00 |
V-2 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 13 November | Partial failure | |||
Apogee: 89 kilometres (55 mi); broke up on re-entry[23] | |||||||
20 November 23:47 |
V-2 | White Sands LC-33 | GE / US Army | ||||
GE[14] | Suborbital | Technology development flight for GE[24] | 20 November | Launch failure, Propulsion trouble at 36 sec.[14] | |||
Apogee: 21 kilometres (13 mi) | |||||||
24 November 17:20 |
Aerobee RTV-N-8 | White Sands LC-35 | US Navy | ||||
Applied Physics Laboratory[16]: Table I, 7.3 | Suborbital | 24 November | Launch failure, off course, flight terminated.[25] | ||||
Apogee: 56 kilometres (35 mi)[11] | |||||||
8 December 21:42 |
V-2 | White Sands LC-33 | GE / US Army | ||||
Blossom II | AMC[14] | Suborbital | Density-pressure-temperature (Michigan University), Skin temperature (Boston University), Solar soft X-rays,Vertical incidence ionosphere propagation, Oblique incidence ionosphere propagation, Aspect project (cameras to be lowered by parachute) (Wright Air Development Center), Sky brightness (AFCRC)[16]: 379–382 (V-2 NO. 28) | 8 December | Successful | ||
Project Hermes launch, apogee: 105 kilometres (65 mi) |
1948
Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
---|---|---|---|---|---|---|---|
Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
Remarks | |||||||
22 January 20:12 |
V-2 | White Sands LC-33 | GE / US Army | ||||
NRL | Suborbital | Chemical release / aeronomy | 22 January | Successful | |||
Project Hermes launch, apogee: 159 kilometres (99 mi)[12] | |||||||
6 February 17:17 |
V-2 | White Sands LC-33 | GE / US Army | ||||
GE | Suborbital | Technology development flight for GE | 6 February | Successful | |||
Project Hermes launch, apogee: 113 kilometres (70 mi)[12] | |||||||
5 March 22:51 |
Aerobee RTV-N-8 | White Sands LC-35 | US Navy | ||||
APL | Suborbital | Chemical release | 5 March | Successful | |||
Apogee: 118 kilometres (73 mi)[11] | |||||||
19 March 23:10 |
V-2 | White Sands LC-33 | GE / US Army | ||||
Blossom IIA | GE | Suborbital | Aeronomy | 19 March | Launch failure | ||
Project Hermes launch, apogee: 5.5 kilometres (3.4 mi)[12] | |||||||
2 April 13:47 |
V-2 | White Sands LC-33 | GE / US Army | ||||
US Army Signal Corps | Suborbital | Aeronomy / Ionosphere / Solar UV | 2 April | Successful | |||
Project Hermes launch, apogee: 144 kilometres (89 mi)[12] | |||||||
13 April 21:41 |
Aerobee RTV-N-8 | White Sands LC-35 | US Navy | ||||
APL | Suborbital | Magnetic field research | 13 April | Successful | |||
Apogee: 114 kilometres (71 mi)[11] | |||||||
19 April 19:54 |
V-2 | White Sands LC-33 | GE / US Army | ||||
NRL | Suborbital | Solar UV / Ionosphere | 19 April | Guidance Failure | |||
Project Hermes launch, apogee: 56 kilometres (35 mi)[12] | |||||||
13 May 13:43 |
Bumper | White Sands LC-33 | GE / US Army | ||||
Bumper 1 | GE | Suborbital | Solar / Ionosphere | 13 May | Successful | ||
Maiden flight of Bumper, apogee: 127.6 kilometres (79.3 mi)[26] | |||||||
27 May 14:15 |
V-2 | White Sands LC-33 | GE / US Army | ||||
APL | Suborbital | Solar UV / Chemical release | 27 May | Successful | |||
Project Hermes launch, apogee: 140 kilometres (87 mi)[12] | |||||||
11 June 10:22 |
V-2 | White Sands LC-33 | GE / US Army | ||||
Blossom III | AMC | Suborbital | Biology / Ionosphere / Aeronomy | 11 June | Launch failure, premature valve closure | ||
Project Hermes launch, apogee: 63 kilometres (39 mi)[12] | |||||||
26 July 16:47 |
Aerobee RTV-N-8 | White Sands LC-35 | US Navy | ||||
APL | Suborbital | Imaging | 26 July | Successful | |||
Apogee: 113 kilometres (70 mi)[11] | |||||||
26 July 18:03 |
V-2 | White Sands LC-33 | GE / US Army | ||||
APL | Suborbital | Chemical release / Aeronomy | 26 July | Successful, Propulsion issues at 45.2s | |||
Project Hermes launch, apogee: 97 kilometres (60 mi)[12] | |||||||
5 August 12:07 |
V-2 | White Sands LC-33 | GE / US Army | ||||
NRL | Suborbital | UV Astronomy / Solar X-ray | 5 August | Successful | |||
Project Hermes launch, apogee: 167 kilometres (104 mi)[12] | |||||||
6 August 1:37 |
Aerobee RTV-N-8 | White Sands LC-35 | US Navy | ||||
NRL | Suborbital | Aeronomy / Solar UV | 6 August | Successful | |||
Apogee: 96.6 kilometres (60.0 mi)[11] | |||||||
19 August 14:45 |
Bumper | White Sands LC-33 | GE / US Army | ||||
Bumper 2 | GE | Suborbital | Solar UV | 19 August | Launch failure | ||
Apogee: 13.1 kilometres (8.1 mi)[26] | |||||||
3 September 01:00 |
V-2 | White Sands LC-33 | GE / US Army | ||||
GRENADES | USASC | Suborbital | Aeronomy | 3 September | Successful | ||
Project Hermes launch, apogee: 151 kilometres (94 mi)[12] | |||||||
17 September | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 17 September | Launch failure[27] | |||
maiden flight of R-1[27] | |||||||
30 September 15:30 |
Bumper | White Sands LC-33 | GE / US Army | ||||
Bumper 3 | GE | Suborbital | Solar UV / X-Ray | 30 September | Launch failure, 2nd Stage Failure | ||
Apogee: 150.6 kilometres (93.6 mi)[26] | |||||||
10 October | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 10 October | Successful[27] | |||
11 October | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test, sounding rocket | 11 October | Successful | |||
First Soviet spaceflight with scientific experiments[27] | |||||||
13 October | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 13 October | Successful[27] | |||
21 October | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 21 October | Successful[27] | |||
23 October | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 23 October | Successful[27] | |||
1 November 14:24 |
Bumper | White Sands LC-33 | GE / US Army[26] | ||||
Bumper 4 | GE | Suborbital | 1 November | Launch failure, tail explosion at 28.5s | |||
Apogee: 5 kilometres (3.1 mi) | |||||||
1 November | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 1 November | Successful[27] | |||
2 November 00:12 |
Aerobee RTV-N-8 | White Sands LC-35 | US Navy | ||||
APL | Suborbital | Cosmic radiation, solar radiation and particles | 2 November | Successful | |||
Apogee: 91 kilometres (57 mi)[11] | |||||||
3 November | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 3 November | Successful[27] | |||
4 November | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 4 November | Successful[27] | |||
5 November | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 5 November | Successful | |||
last of nine launches in the first test series[27] | |||||||
18 November 22:35 |
V-2 | White Sands LC-33 | GE / US Army | ||||
GE | Suborbital | Ramjet research | 18 November | Successful | |||
Project Hermes launch, apogee: 145 kilometres (90 mi)[12] | |||||||
9 December 16:08 |
V-2 | White Sands LC-33 | GE / US Army | ||||
USASC | Suborbital | Aeronomy / Solar X-Ray / Biology | 9 December | Successful | |||
Project Hermes launch, apogee: 108 kilometres (67 mi)[12] | |||||||
9 December 22:38 |
Aerobee XASR-SC-1 | White Sands LC-35 | US Army | ||||
USASC | Suborbital | Aeronomy | 9 December | Successful | |||
Apogee: 91 kilometres (57 mi)[11] |
1949
Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
---|---|---|---|---|---|---|---|
Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
Remarks | |||||||
14 January 20:26 |
V-2 | White Sands LC-33 | US Army | ||||
Hermes II | US Army | Suborbital | Missile test | 14 January | Launch failure | ||
Project Hermes launch, apogee: 1 kilometre (0.62 mi)[28] | |||||||
28 January 17:20 |
V-2 | White Sands LC-33 | GE / US Army | ||||
NRL | Suborbital | Solar x-ray / ionosphere / aeronomy / biology | 28 January | Launch failure | |||
Blossom launch, apogee: 60 kilometres (37 mi)[28] | |||||||
29 January 06:17 |
Aerobee RTV-N-8 | White Sands LC-35 | US Navy | ||||
NRL | Suborbital | Radiation, ionospheric | 29 January | Successful | |||
Apogee: 96.6 kilometres (60.0 mi)[11] | |||||||
1 February 18:38 |
Aerobee RTV-N-8 | White Sands LC-35 | US Navy | ||||
NRL | Suborbital | Solar UV and X-Ray | 1 February | Launch failure | |||
Apogee: 0 kilometres (0 mi)[11] | |||||||
17 February 17:00 |
V-2 | White Sands LC-33 | GE / US Army | ||||
APL | Suborbital | Chemical release / Solar UV / Biology | 17 February | Successful | |||
Apogee: 100.8 kilometres (62.6 mi)[28] | |||||||
24 February 22:14 |
Bumper | White Sands LC-33 | GE / US Army | ||||
Bumper 5 | GE | Suborbital | Aeronomy | 24 February | Successful | ||
Apogee: 393 kilometres (244 mi). The new altitude record.[26] | |||||||
2 March 00:15 |
Aerobee RTV-N-8 | White Sands LC-35 | US Navy | ||||
APL | Suborbital | Test for shipboard launch; dummy payload | 2 March | Launch failure | |||
Apogee: 0 kilometres (0 mi)[11] | |||||||
17 March 23:20 |
Aerobee RTV-N-8 | USS Norton Sound, Pacific Ocean near South America | US Navy | ||||
APL | Suborbital | Ionospheric | 17 March | Successful | |||
Apogee: 105 kilometres (65 mi)[11] | |||||||
22 March 06:43 |
V-2 | White Sands LC-33 | GE / US Army | ||||
Blossom IVA | AMC | Suborbital | Ionospheric | 22 March | Successful | ||
Blossom IVA; apogee: 129 kilometres (80 mi)[28] | |||||||
22 March 17:20 |
Aerobee RTV-N-8 | USS Norton Sound, Pacific Ocean near South America | US Navy | ||||
APL | Suborbital | Ionospheric | 22 March | Successful | |||
Apogee: 105 kilometres (65 mi)[11] | |||||||
24 March 15:14 |
Aerobee RTV-N-8 | USS Norton Sound, Pacific Ocean near South America | US Navy | ||||
APL | Suborbital | Ionospheric | 24 March | Launch failure | |||
Apogee: 5 kilometres (3.1 mi), pressure valve malfunction, booster separated on ignition[11] | |||||||
11 April 22:05 |
V-2 | White Sands LC-33 | GE / US Army | ||||
USASC | Suborbital | Aeronomy / Solar X-Ray / Biology | 11 April | Successful | |||
Apogee: 85 kilometres (53 mi)[28] | |||||||
22 April 00:17 |
Bumper | White Sands LC-33 | GE / US Army | ||||
Bumper 6 | GE | Suborbital | Solar / Aeronomy | 22 April | Launch failure | ||
Apogee: 50 kilometres (31 mi)[26] | |||||||
3 May 16:14 |
Viking (first model) | White Sands LC-33 – Army Launch Area 1 | US Navy | ||||
Viking 1 | NRL | Suborbital | Aeronomy / Imaging | 3 May | Partial launch failure | ||
Apogee: 83 kilometres (52 mi)[6]: 236 [29] | |||||||
5 May 15:15 |
V-2 | White Sands LC-33 | GE / US Army | ||||
GE | Suborbital | Technology development flight for GE / Solar | 5 May | Launch failure | |||
Apogee: 8.9 kilometres (5.5 mi)[28] | |||||||
7 May 03:12 |
R-1A | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 7 May | Successful | |||
Apogee: 109 kilometres (68 mi), maiden flight of R-1A,[10] tested separable warhead | |||||||
10 May 15:57 |
R-1A | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 10 May | Successful | |||
Tested separable warhead[10] | |||||||
15 May 02:48 |
R-1A | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 15 May | Successful | |||
Tested separable warhead[10] | |||||||
16 May 21:55 |
R-1A | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 16 May | Successful | |||
Tested separable warhead[10] | |||||||
24 May 01:40 |
R-1A | Kapustin Yar | NII-88 Section 3 | ||||
FIAR-1 | NII-88 Section 3 | Suborbital | Missile test / Aeronomy | 24 May | Partial Failure | ||
Vertical flight, tested separable warhead, carried aeronomy experiments that were not recovered[10] | |||||||
28 May 01:50 |
R-1A | Kapustin Yar | NII-88 Section 3 | ||||
FIAR-1 | NII-88 Section 3 | Suborbital | Missile test / Aeronomy | 28 May | Partial Failure | ||
Final R1-A flight – vertical flight, tested separable warhead, carried aeronomy experiments damaged on landing and returned no usable data[10] | |||||||
2 June 13:10 |
Aerobee XASR-SC-1 | White Sands LC-35 | US Army | ||||
USASC | Suborbital | Aeronomy | 2 June | Successful | |||
Apogee: 78.4 kilometres (48.7 mi)[11] | |||||||
14 June 22:35 |
V-2 | White Sands LC-33 | GE / US Army | ||||
Blossom IVB | AMC | Suborbital | Biological, Atmospheric | 14 June | Successful | ||
Apogee: 133.9 kilometres (83.2 mi), carried Albert II, first monkey in space[20][30][28] | |||||||
15 June 02:03 |
Aerobee RTV-N-8 | White Sands LC-35 | US Navy | ||||
NRL | Suborbital | Ozone research | 15 June | Successful | |||
Apogee: 109 kilometres (68 mi)[11] | |||||||
17 June 02:03 |
Aerobee RTV-N-8 | White Sands LC-35 | US Navy | ||||
APL | Suborbital | Classified mission | 17 June | Successful | |||
Apogee: 88 kilometres (55 mi)[11] | |||||||
23 June 23:21 |
Aerobee RTV-N-8 | White Sands LC-35 | US Navy | ||||
APL | Suborbital | Solar / Aeronomy | 23 June | Successful | |||
Apogee: 88.5 kilometres (55.0 mi)[11] | |||||||
21 July 16:01 |
Aerobee XASR-SC-1 | White Sands LC-35 | US Army | ||||
USASC | Suborbital | Aeronomy | 21 July | Successful | |||
Apogee: 76.1 kilometres (47.3 mi)[11] | |||||||
6 September 16:57 |
Viking (first model) | White Sands LC-33 – Army Launch Area 1 | US Navy | ||||
Viking 2 | NRL | Suborbital | Aeronomy / Imaging | 6 September | Launch failure | ||
Apogee: 51.5 kilometres (32.0 mi)[6]: 236 [29] | |||||||
10 September | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 10 September | Successful[27] | |||
First flight of second series of tests | |||||||
11 September | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 11 September | Successful[27] | |||
13 September | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 13 September | Successful[27] | |||
14 September | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 14 September | Successful[27] | |||
16 September 23:19 |
V-2 | White Sands LC-33 | GE / US Army | ||||
Blossom IVC | AMC | Suborbital | Biological | 16 September | Launch failure | ||
Apogee: 5 kilometres (3.1 mi), carried Albert III[28] | |||||||
17 September | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 17 September | Successful[27] | |||
19 September | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 19 September | Successful[27] | |||
20 September | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 20 September | Launch failure[27] | |||
20 September 17:03 |
Aerobee XASR-SC-1 | White Sands LC-35 | US Army | ||||
USASC | Suborbital | Aeronomy | 20 September | Successful | |||
Apogee: 58.6 kilometres (36.4 mi)[11] | |||||||
23 September | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 23 September | Launch failure[27] | |||
25 September 11:16 |
R-2E | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 25 September | Successful | |||
Maiden flight of R-2E – a modified R-1 missile to test R-2 concepts: integral fuel tank and separable warhead[31] | |||||||
28 September | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 28 September | Successful[27] | |||
29 September 16:58 |
V-2 | White Sands LC-33 | GE / US Army | ||||
NRL | Suborbital | Ionosphere / Meteorites | 29 September | Successful | |||
Project Hermes launch, apogee: 151.1 kilometres (93.9 mi)[28] | |||||||
30 September 11:49 |
R-2E | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 30 September | Successful[31] | |||
2 October 11:00 |
R-2E | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 2 October | Partial failure | |||
Fire in tail compartment[31] | |||||||
3 October | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 3 October | Successful[27] | |||
6 October | V-2 | White Sands LC-33 | US Army | ||||
Hermes II | US Army | Suborbital | Missile test | 6 October | Launch failure | ||
Project Hermes launch, apogee: 4 kilometres (2.5 mi)[28] | |||||||
8 October 06:05 |
R-2E | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 8 October | Successful[31] | |||
8 October | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 8 October | Successful[27] | |||
10 October | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 10 October | Successful[27] | |||
11 October 12:45 |
R-2E | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 11 October | Partial failure | |||
Fire in tail compartment, last of five R-2E launches[31] | |||||||
12 October | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 12 October | Successful[27] | |||
13 October | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 13 October | Successful[27] | |||
13 October | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 13 October | Successful[27] | |||
15 October | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 15 October | Successful[27] | |||
18 October | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 18 October | Successful[27] | |||
19 October | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 19 October | Successful[27] | |||
22 October | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 22 October | Successful[27] | |||
23 October | R-1 | Kapustin Yar | NII-88 Section 3 | ||||
NII-88 Section 3 | Suborbital | Missile test | 23 October | Successful[27] | |||
Last of second series of twenty firings | |||||||
18 November 16:03 |
V-2 | White Sands LC-33 | GE / US Army | ||||
GRENADES | USASC | Suborbital | Aeronomy / Chemical release | 18 November | Successful | ||
Apogee: 124.2 kilometres (77.2 mi)[28] | |||||||
2 December 22:20 |
Aerobee RTV-A-1 | Holloman LC-A | US Air Force | ||||
US Air Force | Suborbital | Solar, imaging, aeronomy | 2 December | Successful | |||
Apogee: 96 kilometres (60 mi), maiden flight of the RTV-A-1[11] | |||||||
6 December 18:32 |
Aerobee XASR-SC-1 | White Sands LC-35 | US Army | ||||
USASC | Suborbital | Air sampling aeronomy mission | 6 December | Successful | |||
Apogee: 64.9 kilometres (40.3 mi)[11] | |||||||
7 December 00:16 |
Aerobee XASR-SC-1 | White Sands LC-35 | US Army | ||||
USASC | Suborbital | Air sampling aeronomy mission | 7 December | Successful | |||
Apogee: 60 kilometres (37 mi)[11] | |||||||
8 December 19:15 |
V-2 | White Sands LC-33 | GE / US Army | ||||
Blossom IVD | AMC | Suborbital | Biological | 8 December | Successful | ||
Apogee: 127 kilometres (79 mi), carried Albert IV[28] | |||||||
15 December 17:10 |
Aerobee RTV-A-1 | Holloman LC-A | US Air Force | ||||
US Air Force | Suborbital | Solar, imaging, aeronomy | 15 December | Launch failure | |||
Apogee: 0.3 kilometres (0.19 mi)[11] |
1950
Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
---|---|---|---|---|---|---|---|
Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
Remarks | |||||||
15 January 23:45 |
Aerobee RTV-N-10 | USS Norton Sound, Bering Sea | US Navy | ||||
Applied Physics Laboratory | Suborbital | Particle physics | 15 January | Successful | |||
Ship-launched; Apogee: 72 kilometres (45 mi), maiden flight of the RTV-N-10[11] | |||||||
18 January 23:17 |
Aerobee RTV-N-10 | USS Norton Sound, Bering Sea | US Navy | ||||
APL | Suborbital | Particle physics | 18 January | Successful | |||
Ship-launched; Apogee: 80 kilometres (50 mi)[11] | |||||||
9 February 21:44 |
Viking (first model) | White Sands LC-33 – Army Launch Area 1 | US Navy | ||||
Viking 3 | NRL | Suborbital | Solar / Imaging | 9 February | Launch failure | ||
Veered off-course, failed to reach space, apogee: 80.5 kilometres (50.0 mi)[6]: 236 [29] | |||||||
14 February 23:14 |
Aerobee RTV-N-8 | White Sands LC-35 | US Navy | ||||
NRL | Suborbital | Cosmic gamma Ionosphere mission | 14 February | Successful | |||
Apogee: 87.6 kilometres (54.4 mi), final flight of the RTV-N-8[11] | |||||||
17 February 18:00 |
V-2 | White Sands LC-33 | GE / US Army | ||||
NRL | Suborbital | Solar x-ray / Chemical release / Aeronomy | 17 February | Successful | |||
Apogee: 148 kilometres (92 mi)[28] | |||||||
22 February 00:54 |
Aerobee XASR-SC-1 | White Sands LC-35 | US Army | ||||
USASC | Suborbital | Aeronomy | 22 February | Successful | |||
Apogee: 49.1 kilometres (30.5 mi)[11] | |||||||
4 March 00:36 |
Aerobee XASR-SC-1 | White Sands LC-35 | US Army | ||||
USASC | Suborbital | Aeronomy | 4 March | Successful | |||
Apogee: 72.4 kilometres (45.0 mi)[11] | |||||||
14 March 20:43 |
Aerobee RTV-A-1 | Holloman LC-A | US Air Force | ||||
US Air Force | Suborbital | Solar radiation | 14 March | Launch failure | |||
Apogee: 3.2 kilometres (2.0 mi)[11] | |||||||
26 April 01:11 |
Aerobee XASR-SC-2 | White Sands LC-35 | US Army | ||||
USASC | Suborbital | Aeronomy | 26 April | Successful | |||
Apogee: 99.5 kilometres (61.8 mi), maiden flight of the XASR-SC-2[11] | |||||||
12 May 03:08 |
Viking (first model) | USS Norton Sound, Pacific Ocean, near Jarvis Island | US Navy | ||||
Viking 4 | US Navy | Suborbital | Ionospheric / Aeronomy | 12 May | Successful | ||
Apogee: 171 kilometres (106 mi)[6]: 236 [29] | |||||||
12 May 12:30 |
Aerobee RTV-N-10 | White Sands LC-35 | US Navy | ||||
APL | Suborbital | Particle physics | 12 May | Successful | |||
Ship-launched; Apogee: 88.1 kilometres (54.7 mi)[11] | |||||||
26 May 19:43 |
Aerobee RTV-A-1 | Holloman LC-A | US Air Force | ||||
US Air Force | Suborbital | Solar radiation | 26 May | Successful | |||
Apogee: 67.6 kilometres (42.0 mi)[11] | |||||||
2 June 17:07 |
Aerobee RTV-A-1 | Holloman LC-A | US Air Force | ||||
US Air Force | Suborbital | Sky brightness research | 2 June | Successful | |||
Apogee: 24.8 kilometres (15.4 mi)[11] | |||||||
20 June 15:38 |
Aerobee RTV-A-1 | Holloman LC-A | US Air Force | ||||
US Air Force | Suborbital | Aeronomy | 20 June | Successful | |||
Apogee: 92.6 kilometres (57.5 mi)[11] | |||||||
14 July 08:39 |
Aerobee XASR-SC-1 | White Sands LC-35 | US Army | ||||
USASC | Suborbital | Aeronomy | 14 July | Successful | |||
Apogee: 69.2 kilometres (43.0 mi)[11] | |||||||
24 July 14:29 |
Bumper | Cape Canaveral Launch Complex 3 | GE / US Army | ||||
Bumper 8 | GE | Suborbital | Low angle speed test | 24 July | Launch failure | ||
First missile launch from Cape Canaveral; apogee: 20 kilometres (12 mi)[26] | |||||||
29 July 11:25 |
Bumper | Cape Canaveral LC-3 | GE / US Army | ||||
Bumper 7 | GE | Suborbital | Low angle speed test | 29 July | Successful | ||
Apogee: 35.2 kilometres (21.9 mi)[26] | |||||||
3 August 23:52 |
Aerobee RTV-N-10 | White Sands LC-35 | US Navy | ||||
NRL | Suborbital | Solar radiation | 3 August | Launch failure | |||
Apogee: 6 kilometres (3.7 mi)[11] | |||||||
17 August 15:45 |
Aerobee RTV-N-10 | White Sands LC-35 | US Navy | ||||
APL | Suborbital | Spectrometry | 17 August | Successful | |||
Apogee: 101 kilometres (63 mi)[11] | |||||||
31 August 17:09 |
V-2 | White Sands LC-33 | GE / US Army | ||||
Blossom IVG | AMC | Suborbital | Biological | 31 August | Successful | ||
Apogee: 137 kilometres (85 mi), carried a mouse[28] | |||||||
1 October | R-2 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | 1 October | Partial failure | |||
maiden flight of R-2 prototype missile; missed target[32] | |||||||
1 October | R-2 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | 1 October | Partial failure | |||
missed target[32] | |||||||
12 October 19:36 |
Aerobee RTV-A-1 | Holloman LC-A | US Air Force | ||||
US Air Force | Suborbital | Photography | 12 October | Successful | |||
Apogee: 91.3 kilometres (56.7 mi)[11] | |||||||
17 October 04:00 |
Aerobee XASR-SC-2 | White Sands LC-35 | US Army | ||||
USASC | Suborbital | Aeronomy | 17 October | Successful | |||
Apogee: 80.5 kilometres (50.0 mi)[11] | |||||||
18 October 04:30 |
Aerobee XASR-SC-2 | White Sands LC-35 | US Army | ||||
USASC | Suborbital | Aeronomy | 18 October | Successful | |||
Apogee: 85 kilometres (53 mi)[11] | |||||||
21 October | R-2 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | 21 October | Partial Failure | |||
missed target[32] | |||||||
26 October 23:02 |
V-2 | White Sands LC-33 | GE / US Army | ||||
Ballistic Research Laboratory | Suborbital | Technology development for NRL | 26 October | Launch failure | |||
Apogee: 8.1 kilometres (5.0 mi)[28] | |||||||
27 October 13:30 |
Aerobee XASR-SC-2 | White Sands LC-35 | US Army | ||||
USASC | Suborbital | Aeronomy | 27 October | Successful | |||
Apogee: 80.2 kilometres (49.8 mi)[11] | |||||||
1 November | R-2 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | 1 November | Partial failure | |||
Missed target[32] | |||||||
1 November | R-2 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | 1 November | Partial failure | |||
Missed target[32] | |||||||
1 November | R-2 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | 1 November | Partial failure | |||
Missed target[32] | |||||||
1 November | R-2 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | 1 November | Partial failure | |||
Missed target[32] | |||||||
1 November | R-2 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | 1 November | Partial failure | |||
missed target[32] | |||||||
2 November 16:29 |
Aerobee RTV-A-1 | Holloman LC-A | US Air Force | ||||
US Air Force | Suborbital | Air glow research | 2 November | Successful | |||
Apogee: 91.8 kilometres (57.0 mi)[11] | |||||||
9 November | V-2 | White Sands LC-33 | US Army | ||||
Hermes II | US Army | Suborbital | Missile test | 9 November | Partial Failure | ||
Project Hermes launch, apogee: 150 kilometres (93 mi), final flight of the Hermes II[33] | |||||||
21 November 17:18 |
Viking (first model) | White Sands LC-33 – Army Launch Area 1 | US Navy | ||||
Viking 5 | NRL | Suborbital | Solar / Ionospheric | 21 November | Successful | ||
Apogee: 174 kilometres (108 mi)[6]: 236 [29] | |||||||
1 December | R-2 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | 1 December | Partial failure | |||
Missed target[32] | |||||||
1 December | R-2 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | 1 December | Partial failure | |||
Missed target[32] | |||||||
1 December | R-2 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | 1 December | Partial failure | |||
Missed target[32] | |||||||
11 December 17:04 |
Aerobee XASR-SC-2 | White Sands LC-35 | US Army | ||||
USASC | Suborbital | Aeronomy | 11 December | Successful | |||
Apogee: 83.9 kilometres (52.1 mi)[11] | |||||||
12 December 04:06 |
Aerobee XASR-SC-2 | White Sands LC-35 | US Army | ||||
USASC | Suborbital | Aeronomy | 12 December | Successful | |||
Apogee: 84 kilometres (52 mi)[11] | |||||||
12 December 07:04 |
Viking (first model) | White Sands LC-33 – Army Launch Area 1 | US Navy | ||||
Viking 6 | NRL | Suborbital | Solar / Ionospheric | 12 December | Launch failure | ||
Apogee: 64 kilometres (40 mi)[6]: 236 [29] | |||||||
12 December 09:10 |
Aerobee XASR-SC-2 | White Sands LC-35 | US Army | ||||
USASC | Suborbital | Aeronomy | 12 December | Successful | |||
Apogee: 77 kilometres (48 mi)[11] | |||||||
12 December 18:26 |
Aerobee RTV-A-1 | Holloman LC-A | ARDC | ||||
ARDC | Suborbital | Aeronomy | 12 December | Successful | |||
Apogee: 108.2 kilometres (67.2 mi)[11] | |||||||
19 December 18:52 |
Aerobee XASR-SC-2 | White Sands LC-35 | US Army | ||||
USASC | Suborbital | Aeronomy | 19 December | Successful | |||
Apogee: 81.9 kilometres (50.9 mi)[11] | |||||||
20 December | R-2 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | 20 December | Partial failure | |||
Final flight of 12 mission prototype series; missed target[32] |
Suborbital launch summary (1945–1950)
By country
Country | Launches | Successes | Failures | Partial failures | |
---|---|---|---|---|---|
United Kingdom | 3 | 2 | 0 | 1 | |
Soviet Union | 64 | 38 | 7 | 19 | |
United States | 120 | 85 | 33 | 2 |
By rocket
Rocket | Country | Launches | Successes | Failures | Partial failures | Remarks |
---|---|---|---|---|---|---|
V-2 / Hermes II | United States | 59 | 40 | 18 | 1 | Maiden flight, first US spaceflight |
Bumper | United States | 8 | 3 | 5 | 0 | Maiden flight, retired |
Viking (first model) | United States | 6 | 2 | 3 | 1 | Maiden flight |
Aerobee RTV-N-8 | United States | 16 | 12 | 4 | 0 | Maiden flight, retired |
Aerobee RTV-N-10 | United States | 5 | 4 | 1 | 0 | Maiden flight |
Aerobee XASR-SC-1 | United States | 9 | 9 | 0 | 0 | Maiden flight |
Aerobee XASR-SC-2 | United States | 8 | 8 | 0 | 0 | Maiden flight |
Aerobee RTV-A-1 | United States | 9 | 7 | 2 | 0 | Maiden flight |
V-2 | United Kingdom | 3 | 2 | 0 | 1 | Maiden flight, retired |
V-2 | Soviet Union | 11 | 4 | 4 | 3 | Maiden flight, retired |
R-1 | Soviet Union | 30 | 27 | 3 | 0 | Maiden flight, first Soviet spaceflight |
R-1A | Soviet Union | 6 | 4 | 0 | 2 | Maiden flight, retired |
R-2E | Soviet Union | 5 | 3 | 0 | 2 | Maiden flight, retired |
R-2 | Soviet Union | 12 | 0 | 0 | 12 | Maiden flight |
See also
References
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