TheViking made its final flight in 1955 | |
| Rockets | |
|---|---|
| Maiden flights | |
| Retirements | |
In 1955, both the United States and theSoviet Union (USSR) announced plans for launching the world's first satellites during theInternational Geophysical Year (IGY) of 1957–58.Project Vanguard, proposed by theUS Navy, won out over theUS Army'sProject Orbiter as the satellite and rocket design to be flown in the IGY. Development ofIntercontinental Ballistic Missiles, theAtlas by the US and theR-7 by the USSR, accelerated, entering the design and construction phase.
Both the US and USSR continued to launch a myriad ofsounding rockets to probe the outer reaches of Earth's atmosphere and to take quick glimpses of the sun beyond the obscuring layers of air. The Aerobee Hi, first launched in April, promised a comparatively low cost alternative to other high altitude sounding rockets. TheState University of Iowa meanwhile experimented with balloon-launchedrockoons on its fourth expedition into theAtlantic Ocean.

TheAerobee family of rockets expanded considerably this year, both in variety and capability. Most significant was the introduction of the Aerobee-Hi, doubling the altitude range of the Aerobeesounding rocket from 125 km (78 mi) to 220 km (140 mi) and increasing the payload carried from 68 kg (150 lb) to 91 kg (201 lb). Able to probe the upper atmosphere, its $30,000 per flight price tag compared favorably to that of its high altitude contemporaries, theViking and theBumper;[1] at least one 1955 Aerobee-Hi flight returned scientific data.[2][a] Other, less capable, Aerobee rockets still lofted instruments beyond the100-kilometer (62 mi) boundary of space (as defined by theWorld Air Sports Federation)[3] returningspectra of the Sun inultraviolet and investigating atmosphericairglow.[4][5][6]
The Viking series of rockets wrapped up with the flight of Viking 12, launched 4 February 1955. Reaching an altitude of 143.5 mi (230.9 km), the rocket's K-25 camera snapped an infrared picture of the Southwestern United States, from the Pacific coast to Phoenix, just after reaching itsapogee.[7]
A number of sounding rockets based on theNike booster (used as the first stage in various anti-aircraft missiles),[8] were developed and launched. Just one, the 5 April Nike-Deacon flight, breached the limits of space. The Soviet Union launched three R-1E sounding rocket variants of itsR-1 missile (a copy of the GermanV-2), all carrying dogs as biological payloads.[b]
a (the mission date has not yet been determined)b (see table below for details and citations)
Members of the State University of Iowa (SUI) physics department embarked September 1955 on their fourth naval expedition into the Atlantic Ocean to survey the distribution ofcosmic rays andauroral radiation by latitude using balloon-launched rockets (rockoons). The team leader wasFrank B. McDonald, formerly of theUniversity of Minnesota. Their vessel was theUSSAshland, aWorld War 2 eraDock landing ship originally used to transport and launchlanding craft andamphibious vehicles. Two research teams with theNaval Research Laboratory also sailed on theAshland. In addition to theDeacon-equipped rockoons that had been used on the prior expeditions, the SUI team experimented withLoki I rockets launched from balloons. The new vehicle worked perfectly, the first being launched 23 September.
This set the stage for the most ambitious missions of the cruise: the launchings of two two-stage Loki I/Deacon rockoons. The first was a failure, the smaller Loki second stage failing to separate from the Deacon. On the second attempt, both stages fired properly. However, two and a half seconds after second stage ignition, telemetry from the rocket abruptly stopped. ProfessorJames Van Allen, head of the SUI physics department, determined that the thin aluminum nosecone on the rocket had melted due to the incredible friction encountered at its speed of more than 8,000 km (5,000 mi) per hour. Had it reached its target altitude, Van Allen later stated, it might well have discovered theVan Allen Belts two and a half years before the missions ofExplorer 1 andExplorer 3. As it turned out, no more Loki/Deacon missions were attempted.[9]: 34, 37–51
The origin of the International Geophysical Year can be traced to theInternational Polar Years held in 1882–1883, then in 1932–1933 and most recently from March 2007 to March 2009. On 5 April 1950, several top scientists (includingLloyd Berkner,Sydney Chapman,S. Fred Singer, andHarry Vestine), met in James Van Allen's living room and suggested that the time was ripe to have a worldwide Geophysical Year instead of a Polar Year, especially considering recent advances in rocketry, radar, and computing.[10] Berkner and Chapman proposed to theInternational Council of Scientific Unions that anInternational Geophysical Year (IGY) be planned for 1957–58, coinciding with an approaching period of maximum solar activity.[11][12] In 1952, the IGY was announced.[13]
In January 1955, Radio Moscow announced that the Soviet Union might be expected to launch a satellite in the near future. This announcement galvanized American space efforts; in the same month, theNational Academy of Sciences' IGY committee established a Technical Panel on Rocketry to evaluate plans to orbit an American satellite. Already under consideration was Project Orbiter,[14]: 25–26 an Army plan to use a slightly modifiedRedstone (a 200 miles (320 km)) range surface-to-surface missile developed the prior year)[15] combined with upper stages employing 31Loki solid-propellant rockets could put a 5 lb (2.3 kg) satellite into orbit, which could be tracked optically.[14]
On 26 May 1955, theU.S. National Security Council also endorsed a satellite program. On 8 June,United States Secretary of DefenseCharles Wilson directed Assistant SecretaryDonald A. Quarles to coordinate the implementation of a satellite program, with theUnited States Department of Defense providing the rocket and launch facilities, and the civilian IGY National Committee producing the satellite and its experimental package, theNational Science Foundation mediating between the two agencies. A committee, under the chairmanship ofHomer J. Stewart ofJet Propulsion Laboratory, was developed to manage the project to evaluate and choose between the available satellite orbiting options. Project Orbiter now had competition in the form of theNaval Research Laboratory (NRL) plan to develop an orbital capability for itsViking rocket (Project Vanguard), even though the Loki upper stage rockets had been replaced with higher poweredSergeants. On 28 July, confident that a satellite could be lofted during the IGY, PresidentDwight D. Eisenhower's press secretary,James Hagerty, announced that a satellite would officially be among the United States' contributions to the IGY. The Soviets responded four days later with their own announcement of a planned IGY satellite launch.[14]: 25–43
By 9 September, the Stewart Committee had chosen the NRL proposal over the Army's citing the Navy's impressive plannedMinitrack communications technology and network as well as both the civilian nature and the greater growth potential of the Viking/Vanguard rocket. The contract authorizing the construction of two more Viking rockets (13 and 14) was expanded to include development of the Vanguard rockets.[14]: 51–58 NRL received the assignment to develop the Vanguard satellite in early October.[9]: 77
In January 1955,Convair was awarded a long-term government contract for the development of theAtlas, America's firstICBM, beginning Phase Three: detail design and development. With the increasing availability of smaller, lighterthermonuclear weapons, the Atlas design could reach a desired range of 5,500 km (3,400 mi) while using just three engines (original plans had contemplated five). Work on the Atlas accelerated in response to a secret report made in February 1955[16]: 191 byJames Rhyne Killian to theNational Security Council on Soviet rocket progress; in December 1955, Atlas was made the highest-priority project in the nation. In addition, after the issuance of the Killian report, a second ICBM, theTitan, was authorized, along with theThorIntermediate-range ballistic missile (IRBM), this latter rocket using many of the systems already being developed for Atlas.[17] All three of these missiles were adapted into workhorse orbital delivery rockets,[18]: 131–137 the Atlas offered as a backup alternative to both the Redstone and the Vanguard as an IGY launching vehicle.[14]: 41
Also authorized in the wake of the Killian report was theU.S. Army'sJupiter IRBM proposal, which was to be jointly developed by theU.S. Navy for use on vessels (the Navy dropped out of the project late the following year). The Jupiter also ultimately became a space launcher under the designationJuno II.[19]

The single-stageR-5 missile completed its test launch series and entered operational service in 1955; it was able to carry the same 1,000 kilograms (2,200 lb) payload as its shorter ranged predecessors, theR-1 andR-2 but over a distance of 1,200 kilometres (750 mi). Work then proceeded on an upgrade designated R-5M, with similar launch mass and range, but designed to carry a nuclear warhead.[20]: 242–243 This rocket, which would be the world's first nuclear missile, was a stopgap weapon pending the development of an ICBM, the development of both of which had been decreed by the USSR Council of Ministers in late 1953.[20]: 275
This ICBM was theR-7, whose design began in 1954. Initially contemplated as a two-stage design, the R-7 ultimately employed a cluster of four strapon boosters around a central rocket (or "sustainer"). For the first time, Soviet engineers were developing a rocket with more than a single combustion chamber (in the case of the R-7, there were32). This ambitious project was the joint effort of three design entities:OKB-1, responsible for the general hydraulic system, NII-885, managing the general electrical system, andOKB-456, developing the engines' layout and thrust sequence.[20]: 290–1 In 1955, after the traditional launch pad proved to be unusable for the R-7, a plan was advanced to suspend the sustainer at the launch site, attaching the strapon cluster there; the entire assembly would be suspended by the launch facility rather than resting on the ground.[20]: 295 The first test launches were planned for 1957. The site for these launches, decided 12 February 1955, was Ministry of Defense Scientific-Research and Test Firing Range No.5 (NIIP-5), located in theKazakh Soviet Socialist Republic (nowKazakhstan) near theSyr-Darya river. The town ofBaikonur grew to support the facility.[20]: 308
Though the R-7 was developed explicitly as a nuclear missile,OKB-1's headSergei Korolev already had plans to utilize the rocket for delivering satellites into orbit. At a private meeting on 30 August 1955, Korolev proposed this possibility Vasily Ryabikov, chairman of the Military Industrial Meeting. This suggestion culminated in the governmental resolution of January 1956 calling for the production of the Soviet Union's first satellite.[20]: 380
| Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
|---|---|---|---|---|---|---|---|
| Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
| Remarks | |||||||
| 4 January | |||||||
| OKB-1 | Suborbital | Missile test | 4 January | Successful[21] | |||
| 6 January | |||||||
| OKB-1 | Suborbital | Missile test | 6 January | Successful[22] | |||
| 8 January | |||||||
| OKB-1 | Suborbital | Missile test | 8 January | Successful[22] | |||
| 15 January | |||||||
| OKB-1 | Suborbital | Missile test | 15 January | Successful[21] | |||
| 17 January | |||||||
| OKB-1 | Suborbital | Missile test | 17 January | Successful[22] | |||
| 20 January | |||||||
| OKB-1 | Suborbital | Missile test | 20 January | Successful | |||
| Maiden flight of the R-5M[22] | |||||||
| 21 January | |||||||
| OKB-1 | Suborbital | Missile test | 21 January | Successful[22] | |||
| 22 January 00:54 | USAF 51 | ||||||
| AFCRC | Suborbital | Aeronomy | 22 January | Successful | |||
| Apogee: 94.8 kilometres (58.9 mi)[23]: 145–146 | |||||||
| 22 January | |||||||
| OKB-1 | Suborbital | Missile test | 22 January | Successful[22] | |||
| 25 January | |||||||
| OKB-1 | Suborbital | Biological | 25 January | Successful | |||
| Maiden flight of the R-1E, carried dogs[24] | |||||||
| 25 January | |||||||
| OKB-1 | Suborbital | Missile test | 25 January | Successful[21] | |||
| 28 January | |||||||
| OKB-1 | Suborbital | Missile test | 28 January | Successful[25] | |||
| 29 January | |||||||
| OKB-1 | Suborbital | Missile test | 29 January | Successful[25] | |||
| 29 January | |||||||
| OKB-1 | Suborbital | Missile test | 29 January | Successful[22] | |||
| 31 January | |||||||
| OKB-1 | Suborbital | Missile test | 31 January | Successful[21] | |||
| Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
|---|---|---|---|---|---|---|---|
| Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
| Remarks | |||||||
| 1 February | |||||||
| OKB-1 | Suborbital | Missile test | 1 February | Successful[22] | |||
| 3 February | |||||||
| OKB-1 | Suborbital | Missile test | 3 February | Successful[25] | |||
| 4 February 21:55 | |||||||
| NRL | Suborbital | REV test / Photography / Aeronomy | 4 February | Successful | |||
| Apogee: 232 kilometres (144 mi)[26] | |||||||
| 5 February | |||||||
| OKB-1 | Suborbital | Biological | 5 February | Partial Failure | |||
| Carried dogs, not recovered[24] | |||||||
| 7 February | |||||||
| OKB-1 | Suborbital | Missile test | 7 February | Successful[25] | |||
| 7 February | |||||||
| OKB-1 | Suborbital | Missile test | 7 February | Successful[22] | |||
| 7 February 18:51 | USAF 52 | ||||||
| AFCRC /University of Utah | Suborbital | Ionospheric | 7 February | Successful | |||
| Apogee: 120.4 kilometres (74.8 mi)[23]: 147–148 | |||||||
| 8 February | |||||||
| OKB-1 | Suborbital | Missile test | 8 February | Successful[21] | |||
| 8 February | |||||||
| OKB-1 | Suborbital | Missile test | 8 February | Successful[21] | |||
| 9 February | |||||||
| OKB-1 | Suborbital | Missile test | 9 February | Successful[22] | |||
| 10 February 22:38 | USAF 53 | ||||||
| AFCRC / University of Utah | Suborbital | Ionospheric | 10 February | Successful | |||
| Apogee: 76.1 kilometres (47.3 mi)[23]: 149–150 | |||||||
| 14 February | |||||||
| OKB-1 | Suborbital | Missile test | 14 February | Successful[22] | |||
| 21 February 18:25 | NRL 29 | ||||||
| NRL | Suborbital | Solar UV | 21 February | Successful | |||
| Apogee: 115 kilometres (71 mi), maiden flight of the RTV-N-10c;[27] obtained UV spectrum in 30 second exposure over range 977 to 1817A. UsedUniversity of Colorado biaxial pointer to keep camera trained on the Sun.[4] | |||||||
| 25 February | |||||||
| OKB-1 | Suborbital | Missile test | 25 February | Successful[21] | |||
| 28 February | |||||||
| OKB-1 | Suborbital | Missile test | 28 February | Successful[21] | |||
| Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
|---|---|---|---|---|---|---|---|
| Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
| Remarks | |||||||
| 1 March | |||||||
| OKB-1 | Suborbital | Missile test | 1 March | Successful[21] | |||
| 2 March | |||||||
| OKB-1 | Suborbital | Missile test | 2 March | Successful[21] | |||
| 19 March 06:00 | NRL 26 | ||||||
| NRL | Suborbital | Airglow | 19 March | Successful | |||
| Apogee: 115 kilometres (71 mi)[27] | |||||||
| 21 March | |||||||
| OKB-1 | Suborbital | Missile test | 21 March | Successful[21] | |||
| 29 March 16:47 | USAF 54 | ||||||
| AFCRC /University of Colorado | Suborbital | Solar UV | 29 March | Successful | |||
| Apogee: 113 kilometres (70 mi)[23]: 151–152 | |||||||
| Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
|---|---|---|---|---|---|---|---|
| Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
| Remarks | |||||||
| 4 April | |||||||
| OKB-1 | Suborbital | Missile test | 4 April | Successful[21] | |||
| 8 April | |||||||
| OKB-1 | Suborbital | Missile test | 8 April | Successful[25] | |||
| 8 April | |||||||
| NACA | Suborbital | REV test | 8 April | Launch failure | |||
| Apogee: 18 kilometres (11 mi), maiden (and only) flight of the Nike-Nike-Tri-Deacon-T40[28] | |||||||
| 8 April 15:19 | DAN-1 | ||||||
| US Air Force | Suborbital | Test flight | 8 April | Successful | |||
| Apogee: 108 kilometres (67 mi), maiden flight of the Nike-Deacon[29] | |||||||
| 9 April | |||||||
| OKB-1 | Suborbital | Missile test | 9 April | Successful[25] | |||
| 12 April | |||||||
| OKB-1 | Suborbital | Missile test | 12 April | Successful[25] | |||
| 15 April | |||||||
| OKB-1 | Suborbital | Missile test | 15 April | Successful[25] | |||
| 21 April 15:58 | USAF 55 | ||||||
| AFCRC | Suborbital | Test flight | 21 April | Successful | |||
| Apogee: 192 kilometres (119 mi), maiden flight of the AJ11-6 Aerobee Hi (USAF variant)[23]: 153–154 | |||||||
| 29 April | |||||||
| OKB-1 | Suborbital | Missile test | 29 April | Partial Failure[22] | |||
| Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
|---|---|---|---|---|---|---|---|
| Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
| Remarks | |||||||
| 18 May | |||||||
| OKB-1 | Suborbital | Missile test | 18 May | Successful[21] | |||
| 20 May | |||||||
| OKB-1 | Suborbital | Missile test | 20 May | Successful[21] | |||
| 20 May | |||||||
| OKB-1 | Suborbital | Missile test | 20 May | Successful[22] | |||
| 26 May | |||||||
| OKB-1 | Suborbital | Missile test | 26 May | Successful[22] | |||
| 28 May | |||||||
| OKB-1 | Suborbital | Missile test | 28 May | Successful[21] | |||
| 31 May | |||||||
| OKB-1 | Suborbital | Missile test | 31 May | Successful[21] | |||
| Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
|---|---|---|---|---|---|---|---|
| Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
| Remarks | |||||||
| 1 June | |||||||
| OKB-1 | Suborbital | Missile test | 1 June | Successful[21] | |||
| 6 June | |||||||
| OKB-1 | Suborbital | Missile test | 6 June | Successful[22] | |||
| 15 June | |||||||
| OKB-1 | Suborbital | Missile test | 15 June | Successful[22] | |||
| 16 June 01:11 | USAF 56 | ||||||
| Holloman Air Development Center | Suborbital | Classified | 16 June | Successful | |||
| Apogee: 203 kilometres (126 mi), maiden flight of the Aerobee AJ10-27[23]: 157 | |||||||
| 18 June | |||||||
| OKB-1 | Suborbital | Missile test | 18 June | Successful[25] | |||
| 20 June | |||||||
| OKB-1 | Suborbital | Missile test | 20 June | Successful[21] | |||
| 22 June | |||||||
| OKB-1 | Suborbital | Missile test | 22 June | Successful[22] | |||
| 23 June | |||||||
| OKB-1 | Suborbital | Missile test | 23 June | Successful[22] | |||
| 23 June | |||||||
| NACA | Suborbital | Heat transfer REV test | 23 June | Launch failure | |||
| Apogee: 30 kilometres (19 mi)[30] | |||||||
| 23 June 12:47 | USAF 57 | ||||||
| AFCRC | Suborbital | Test flight | 23 June | Launch failure | |||
| Apogee: 61 kilometres (38 mi), premature burnout at 23 seconds[23]: 155–156 | |||||||
| 24 June | |||||||
| OKB-1 | Suborbital | Missile test | 24 June | Successful[25] | |||
| 24 June 18:04 | DAN-2 | ||||||
| NACA | Suborbital | Aeronomy | 24 June | Successful | |||
| Apogee: 105 kilometres (65 mi)[29] | |||||||
| 28 June | |||||||
| OKB-1 | Suborbital | Missile test | 28 June | Successful[21] | |||
| 28 June | |||||||
| OKB-1 | Suborbital | Missile test | 28 June | Successful[22] | |||
| 30 June | |||||||
| OKB-1 | Suborbital | Missile test | 30 June | Successful[22] | |||
| Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
|---|---|---|---|---|---|---|---|
| Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
| Remarks | |||||||
| 1 July | |||||||
| OKB-1 | Suborbital | Missile test | 1 July | Successful[21] | |||
| 7 July | |||||||
| OKB-1 | Suborbital | Missile test | 7 July | Successful[22] | |||
| 8 July 08:39 | NRL 23 | ||||||
| NRL | Suborbital | Ionospheric | 8 July | Successful | |||
| Apogee: 113 kilometres (70 mi)[27] | |||||||
| 9 July | |||||||
| OKB-1 | Suborbital | Missile test | 9 July | Successful[22] | |||
| 13 July 06:59 | NRL 23 | ||||||
| NRL | Suborbital | Aeronomy | 13 July | Successful | |||
| Apogee: 69 kilometres (43 mi), maiden flight of the Aerobee RTV-N-10a[27] | |||||||
| 15 July | |||||||
| OKB-1 | Suborbital | Missile test | 15 July | Successful[21] | |||
| 25 July | |||||||
| OKB-1 | Suborbital | Missile test | 25 July | Successful[25] | |||
| 26 July | |||||||
| OKB-1 | Suborbital | Missile test | 26 July | Successful[25] | |||
| 26 July | |||||||
| OKB-1 | Suborbital | Missile test | 26 July | Successful[21] | |||
| 29 July | |||||||
| OKB-1 | Suborbital | Missile test | 29 July | Successful[25] | |||
| Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
|---|---|---|---|---|---|---|---|
| Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
| Remarks | |||||||
| 1 August | |||||||
| OKB-1 | Suborbital | Missile test | 1 August | Successful[25] | |||
| 1 August | |||||||
| OKB-1 | Suborbital | Missile test | 1 August | Successful[21] | |||
| 3 August | |||||||
| OKB-1 | Suborbital | Missile test | 3 August | Successful[21] | |||
| 6 August | |||||||
| OKB-1 | Suborbital | Missile test | 6 August | Successful[21] | |||
| 8 August | |||||||
| OKB-1 | Suborbital | Missile test | 8 August | Successful[21] | |||
| 9 August | |||||||
| OKB-1 | Suborbital | Missile test | 9 August | Successful[22] | |||
| 12 August | |||||||
| OKB-1 | Suborbital | Missile test | 12 August | Successful[22] | |||
| 16 August | |||||||
| OKB-1 | Suborbital | Missile test | 16 August | Partial Failure[22] | |||
| 24 August | |||||||
| OKB-1 | Suborbital | Missile test | 24 August | Successful[25] | |||
| 24 August | |||||||
| OKB-1 | Suborbital | Missile test | 24 August | Successful[21] | |||
| 25 August | |||||||
| OKB-1 | Suborbital | Missile test | 25 August | Successful[25] | |||
| 25 August 13:00 | NRL 37 | ||||||
| NRL | Suborbital | Test flight | 25 August | Launch failure | |||
| Apogee: 4 kilometres (2.5 mi), maiden flight of the Aerobee Hi (NRL variant), Navy designation: RTV-N-13[27] | |||||||
| 26 August | |||||||
| ARDC | Suborbital | Test flight | 26 August | Launch failure | |||
| Apogee: 3 kilometres (1.9 mi), maiden flight of the X-17[31] | |||||||
| 27 August | |||||||
| OKB-1 | Suborbital | Missile test | 27 August | Successful[21] | |||
| 30 August | |||||||
| OKB-1 | Suborbital | Missile test | 30 August | Successful[21] | |||
| 31 August | |||||||
| OKB-1 | Suborbital | Missile test | 31 August | Successful[21] | |||
| Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
|---|---|---|---|---|---|---|---|
| Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
| Remarks | |||||||
| 14 September 13:30 | USAF 58 | ||||||
| AFCRC /University of Michigan | Suborbital | Aeronomy | 14 September | Successful | |||
| Apogee: 95 kilometres (59 mi)[23]: 158–159 | |||||||
| 15 September | |||||||
| NACA | Suborbital | Test flight | 15 September | Launch failure | |||
| Apogee: 10 kilometres (6.2 mi), maiden flight of the HJ-Nike[32] | |||||||
| 19 September | |||||||
| OKB-1 | Suborbital | Missile test | 19 September | Successful[22] | |||
| 23 September | |||||||
| OKB-1 | Suborbital | Missile test | 23 September | Successful[22] | |||
| 23 September | |||||||
| ARDC | Suborbital | Test flight | 23 September | Launch failure | |||
| Apogee: 5 kilometres (3.1 mi)[31] | |||||||
| 23 September 20:34 | SUI 38 | ||||||
| University of Iowa | Suborbital | Ionospheric / Aeronomy | 23 September | Successful | |||
| Apogee: 100 kilometres (62 mi)[33] | |||||||
| 24 September 16:35 | SUI 39 | ||||||
| University of Iowa | Suborbital | Ionospheric / Aeronomy | 24 September | Successful | |||
| Apogee: 100 kilometres (62 mi)[34] | |||||||
| 24 September 21:09 | SUI 40 | ||||||
| University of Iowa | Suborbital | Ionospheric / Aeronomy | 24 September | Successful | |||
| Apogee: 100 kilometres (62 mi)[33] | |||||||
| 25 September 20:39 | SUI 41 | ||||||
| University of Iowa | Suborbital | Ionospheric / Aeronomy | 25 September | Launch failure | |||
| Apogee: 11 kilometres (6.8 mi)[33] | |||||||
| 27 September | |||||||
| OKB-1 | Suborbital | Missile test | 27 September | Successful[22] | |||
| 27 September | |||||||
| NACA | Suborbital | REV test flight | 27 September | Successful | |||
| Apogee: 30 kilometres (19 mi)[29] | |||||||
| 27 September 19:12 | NRL Rockoon 14 | ||||||
| NRL | Suborbital | Ionospheric / Aeronomy | 27 September | Launch failure | |||
| Apogee: 11 kilometres (6.8 mi)[34] | |||||||
| 27 September 19:43 | NRL Rockoon 13 | ||||||
| NRL | Suborbital | Ionospheric / Aeronomy | 27 September | Successful | |||
| Apogee: 90 kilometres (56 mi)[34] | |||||||
| 27 September 20:54 | SUI 42 | ||||||
| University of Iowa | Suborbital | Ionospheric / Aeronomy | 27 September | Successful | |||
| Apogee: 100 kilometres (62 mi)[34] | |||||||
| 28 September 01:13 | SUI 43 | ||||||
| University of Iowa | Suborbital | Ionospheric / Aeronomy | 28 September | Launch failure | |||
| Apogee: 100 kilometres (62 mi)[33] | |||||||
| 28 September 12:45 | NRL Rockoon 15 | ||||||
| NRL | Suborbital | Ionospheric / Aeronomy | 28 September | Successful | |||
| Apogee: 90 kilometres (56 mi)[34] | |||||||
| 28 September 14:54 | SUI 44 | ||||||
| University of Iowa | Suborbital | Ionospheric / Aeronomy | 28 September | Successful | |||
| Apogee: 100 kilometres (62 mi)[34] | |||||||
| 28 September 17:40 | NRL Rockoon 16 | ||||||
| NRL | Suborbital | Ionospheric / Aeronomy | 28 September | Launch failure | |||
| Apogee: 11 kilometres (6.8 mi)[34] | |||||||
| 28 September 19:22 | SUI 45 | ||||||
| University of Iowa | Suborbital | Test flight | 28 September | Launch failure | |||
| Apogee: 102 kilometres (63 mi), maiden flight of the Deacon-Loki rockoon[35] | |||||||
| 29 September | |||||||
| OKB-1 | Suborbital | Missile test | 29 September | Successful[21] | |||
| 29 September 13:42 | SUI 46 | ||||||
| University of Iowa | Suborbital | Ionospheric / Aeronomy | 29 September | Successful | |||
| Apogee: 100 kilometres (62 mi)[34] | |||||||
| 29 September 19:13 | SUI 47 | ||||||
| University of Iowa | Suborbital | Ionospheric / Aeronomy | 29 September | Successful | |||
| Apogee: 100 kilometres (62 mi)[34] | |||||||
| 29 September 21:52 | SUI 48 | ||||||
| University of Iowa | Suborbital | Test flight | 29 September | Launch failure | |||
| Apogee: 100 kilometres (62 mi), final flight of the Deacon-Loki rockoon[35] | |||||||
| 30 September 15:50 | USAF 59 | ||||||
| AFCRC /University of Utah /University of Colorado | Suborbital | Solar UV | 30 September | Successful | |||
| Apogee: 74 kilometres (46 mi)[23]: 160–161 | |||||||
| 30 September 20:10 | SUI 49 | ||||||
| University of Iowa | Suborbital | Ionospheric / Aeronomy | 30 September | Successful | |||
| Apogee: 100 kilometres (62 mi)[33] | |||||||
| Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
|---|---|---|---|---|---|---|---|
| Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
| Remarks | |||||||
| 1 October | |||||||
| OKB-1 | Suborbital | Missile test | 1 October | Successful[21] | |||
| 1 October | |||||||
| OKB-1 | Suborbital | Missile test | 1 October | Successful[22] | |||
| 4 October 21:18 | SUI 50 | ||||||
| University of Iowa | Suborbital | Ionospheric / Aeronomy | 4 October | Successful | |||
| Apogee: 100 kilometres (62 mi)[33] | |||||||
| 5 October | |||||||
| OKB-1 | Suborbital | Missile test | 5 October | Successful[25] | |||
| 6 October 10:45 | NRL Rockoon 17 | ||||||
| NRL | Suborbital | Ionospheric / Aeronomy | 6 October | Launch failure | |||
| Apogee: 11 kilometres (6.8 mi)[34] | |||||||
| 6 October 19:10 | SUI 51 | ||||||
| University of Iowa | Suborbital | Ionospheric / Aeronomy | 6 October | Successful | |||
| Apogee: 100 kilometres (62 mi)[34] | |||||||
| 7 October | |||||||
| NACA | Suborbital | Heat transfer REV test | 7 October | Successful | |||
| Apogee: 30 kilometres (19 mi)[30] | |||||||
| 8 October | |||||||
| OKB-1 | Suborbital | Missile test | 8 October | Successful[25] | |||
| 11 October 14:33 | SUI 52 | ||||||
| University of Iowa | Suborbital | Ionospheric / Aeronomy | 11 October | Launch failure | |||
| Apogee: 20 kilometres (12 mi)[34] | |||||||
| 11 October 14:37 | NRL Rockoon 18 | ||||||
| NRL | Suborbital | Ionospheric / Aeronomy | 11 October | Successful | |||
| Apogee: 90 kilometres (56 mi)[34] | |||||||
| 13 October 01:00 | USAF 60 | ||||||
| AFCRC | Suborbital | Aeronomy | 13 October | Successful | |||
| Apogee: 101 kilometres (63 mi)[23]: 162–163 | |||||||
| 13 October 06:37 | NRL Rockoon 19 | ||||||
| NRL | Suborbital | Ionospheric / Aeronomy | 13 October | Successful | |||
| Apogee: 60 kilometres (37 mi)[34] | |||||||
| 13 October 12:44 | SUI 53 | ||||||
| University of Iowa | Suborbital | Ionospheric / Aeronomy | 13 October | Successful | |||
| Apogee: 100 kilometres (62 mi)[34] | |||||||
| 13 October 13:42 | NRL Rockoon 20 | ||||||
| NRL | Suborbital | Ionospheric / Aeronomy | 13 October | Launch failure | |||
| Apogee: 50 kilometres (31 mi)[34] | |||||||
| 13 October 15:24 | SUI 54 | ||||||
| University of Iowa | Suborbital | Ionospheric / Aeronomy | 13 October | Launch failure | |||
| Apogee: 20 kilometres (12 mi)[34] | |||||||
| 13 October 20:13 | SUI 55 | ||||||
| University of Iowa | Suborbital | Ionospheric / Aeronomy | 13 October | Successful | |||
| Apogee: 100 kilometres (62 mi)[34] | |||||||
| 18 October 22:49 | NRL 34 | ||||||
| NRL | Suborbital | Solar UV / Solar X-Ray | 18 October | Successful | |||
| Apogee: 101 kilometres (63 mi)[27] | |||||||
| 22 October 00:20 | NRL 35 | ||||||
| NRL | Suborbital | Solar UV | 22 October | Successful | |||
| Apogee: 185 kilometres (115 mi)[27] | |||||||
| 31 October | |||||||
| OKB-1 | Suborbital | Missile test | 31 October | Successful[21] | |||
| Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
|---|---|---|---|---|---|---|---|
| Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
| Remarks | |||||||
| 1 November | |||||||
| OKB-1 | Suborbital | Missile test | 1 November | Successful[22] | |||
| 4 November | |||||||
| OKB-1 | Suborbital | Biological | 4 November | Successful | |||
| Carried dogs, all recovered[24] | |||||||
| 4 November | |||||||
| OKB-1 | Suborbital | Missile test | 4 November | Successful[22] | |||
| 4 November 15:30 | NRL 36 | ||||||
| NRL | Suborbital | Solar UV | 4 November | Successful | |||
| Apogee: 135 kilometres (84 mi)[27] | |||||||
| 17 November 09:15 | NRL 25 | ||||||
| NRL | Suborbital | Meteorites / UV Astronomy | 17 November | Successful | |||
| Apogee: 105 kilometres (65 mi)[27] | |||||||
| 19 November | |||||||
| OKB-1 | Suborbital | Missile test | 19 November | Successful[21] | |||
| 19 November | |||||||
| OKB-1 | Suborbital | Missile test | 19 November | Successful[22] | |||
| 23 November | |||||||
| OKB-1 | Suborbital | Missile test | 23 November | Successful[21] | |||
| 23 November | |||||||
| OKB-1 | Suborbital | Missile test | 23 November | Successful[21] | |||
| 29 November 17:16 | NRL 24 | ||||||
| NRL | Suborbital | Ionospheric | 29 November | Successful | |||
| Apogee: 132 kilometres (82 mi)[27] | |||||||
| Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
|---|---|---|---|---|---|---|---|
| Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
| Remarks | |||||||
| 1 December | |||||||
| ARDC | Suborbital | Test flight | 1 December | Successful | |||
| Apogee: 100 kilometres (62 mi)[31] | |||||||
| 9 December 14:50 | NRL 38 | ||||||
| NRL | Suborbital | Test flight | 9 December | Launch failure[27] | |||
| 13 December 05:00 | NRL 28 | ||||||
| NRL | Suborbital | Airglow / Aeronomy | 13 December | Successful | |||
| Apogee: 142 kilometres (88 mi), final flight of the Aerobee RTV-N-10a;[27] carriedphotometers to measure altitude and intensity ofairglow at 5577 and 5890-6A.[5] Also took threeultravioletspectrograms of the Sun, investigatingLy-α emissions.[6] | |||||||
| 13 December 17:58 | USAF 61 | ||||||
| AFCRC /University of Utah /University of Colorado | Suborbital | Solar UV | 13 December | Successful | |||
| Apogee: 138 kilometres (86 mi), final flight of the Aerobee AJ10-27[23]: 164–165 | |||||||
| 16 December | |||||||
| OKB-1 | Suborbital | Missile test | 16 December | Successful[21] | |||
| 17 December | |||||||
| OKB-1 | Suborbital | Missile test | 17 December | Successful[21] | |||
| 21 December | |||||||
| NACA | Suborbital | Test flight | 21 December | Launch failure | |||
| Apogee: 10 kilometres (6.2 mi)[32] | |||||||
| 24 December | |||||||
| OKB-1 | Suborbital | Missile test | 24 December | Successful[21] | |||
| 27 December | |||||||
| OKB-1 | Suborbital | Missile test | 27 December | Successful[21] | |||
| 28 December | |||||||
| OKB-1 | Suborbital | Missile test | 28 December | Successful[21] | |||
| 30 December | |||||||
| OKB-1 | Suborbital | Missile test | 30 December | Successful[21] | |||
| Country | Launches | Successes | Failures | Partial failures | |
|---|---|---|---|---|---|
| 95 | 92 | 0 | 3 | ||
| 61 | 42 | 19 | 0 | ||
| World | 156 | 134 | 19 | 3 | |
| Rocket | Country | Launches | Successes | Failures | Partial failures | Remarks |
|---|---|---|---|---|---|---|
| Viking (second model) | 1 | 1 | 0 | 0 | ||
| Aerobee RTV-N-10 | 4 | 4 | 0 | 0 | ||
| Aerobee RTV-N-10c | 4 | 4 | 0 | 0 | Maiden flight | |
| Aerobee RTV-N-10a | 2 | 2 | 0 | 0 | Maiden flight, retired | |
| Aerobee Hi (NRL) | 2 | 0 | 2 | 0 | Maiden flight | |
| Aerobee RTV-A-1a | 5 | 5 | 0 | 0 | ||
| Aerobee Hi (USAF) | 2 | 1 | 1 | 0 | Maiden flight | |
| Aerobee AJ10-27 | 4 | 4 | 0 | 0 | Maiden flight, retired | |
| Deaconrockoon (SUI) | 10 | 8 | 2 | 0 | ||
| Deaconrockoon (NRL) | 8 | 4 | 4 | 0 | ||
| Lokirockoon | 6 | 4 | 2 | 0 | Maiden flight | |
| Deacon-Lokirockoon | 2 | 0 | 2 | 0 | Maiden flight, retired | |
| Nike-Nike-T40-T55 | 2 | 1 | 1 | 0 | ||
| Nike-Deacon | 3 | 3 | 0 | 0 | Maiden flight | |
| Nike-Nike-Tri-Deacon-T40 | 1 | 0 | 1 | 0 | Maiden flight, retired | |
| X-17 | 3 | 1 | 2 | 0 | Maiden flight | |
| HJ-Nike | 2 | 0 | 2 | 0 | Maiden flight | |
| R-1 | 18 | 18 | 0 | 0 | ||
| R-1E | 3 | 2 | 0 | 1 | Maiden flight | |
| R-2 | 42 | 42 | 0 | 0 | ||
| R-5 | 8 | 8 | 0 | 0 | ||
| R-5M | 24 | 22 | 0 | 2 | Maiden flight |