1952 in spaceflight
Template:Short description Script error: No such module "Category handler".Script error: No such module "Check for unknown parameters".
Template:Use American English Script error: No such module "Unsubst". Template:Infobox Year in spaceflight Template:Infobox spaceflight
Script error: No such module "Navbox".
In 1952, several branches of the United States' military, often in partnership with civilian organizations, continued their programs of sounding rocket research beyond the Script error: No such module "convert". boundary of space (as defined by the World Air Sports Federation)[1] using the Aerobee rocket. The University of Iowa launched its first series of rockoon flights, demonstrating the validity of the balloon-launched rocket, a comparatively inexpensive way to explore the upper atmosphere. The launch of Viking 9 at the end of the year to an altitude of Template:Cvt, by the Naval Research Laboratory team under the management of Milton Rosen, represented the pinnacle of contemporary operational rocket design.
The same year, groundwork was laid for the launch of the first artificial satellite when, in October, the General Assembly of the International Council of Scientific Unions (ICSU) scheduled the International Geophysical Year for 1957–58. This scientific endeavor would involve 67 nations in a global investigation of physical phenomena, on the ground and in space.
No new models of ballistic missile were added to the arsenals of either the United States or the Soviet Union in 1952. However, work continued on large rocket development, particularly the US Army's Redstone and the Soviet R-5 missile. Both the R-1 and R-2 missiles had operational test runs during the year.
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Space exploration highlights
In the late spring of 1952, the Naval Research Laboratory team, under the management of Milton Rosen, prepared to launch the first second-generation Viking rocket, Viking 8, from the White Sands Missile Range in New Mexico. The new Viking design was nearly one-and-a-half times as wide as its precursor, with the highest fuel-to-weight ratio of any rocket yet developed. The tail fins no longer supported the weight of the rocket, which had been the case with the first-generation design. Now, the Viking rocket rested on the base of its fuselage. This allowed the tail fins to be made much lighter, allowing the rocket to carry a heavier tank without weighing more than the first Viking design.[2]Template:Rp
On 6 June 1952, Viking 8 broke loose of its moorings during a static firing test. After it was allowed to fly for 55 seconds in the hope that it would clear the immediate area and thus pose no danger to ground crew, Nat Wagner, head of the "Cutoff group", delivered a command to the rocket to cease its thrust. 65 seconds later, the rocket crashed Script error: No such module "convert". downrange to the southeast.[2]Template:Rp
With lessons learned from the Viking 8 failure, the successful 9 December static firing of Viking 9 was followed on 15 December by a successful launch from White Sands. The rocket reached an altitude of Script error: No such module "convert"., roughly the same as that of the first-generation Viking 7 in 1950. In addition to cameras that photographed the Earth during flight, Viking 9 carried a full suite of cosmic ray, ultraviolet, and X-ray detectors, including sixteen plates of emulsion gel for tracking the path of individual high energy particles. The experiment package was recovered intact after it had secured measurements high above the Earth's atmosphere.[2]Template:Rp
US Army
The final flight of the V-2 rocket occurred on 19 September 1952 with an unsuccessful aeronomy mission conducted jointly by the Signal Corps Engineering Laboratories and University of Michigan from White Sands Launch Complex 33. The rocket reached an apogee of Script error: No such module "convert". before its tail exploded 27 seconds into the flight.[3]Template:Rp
American civilian efforts
1952 saw the first rockoon flights. These balloon-mounted rockets were significantly cheaper than sounding rocket flights: $1800 per launch versus $25,000 for each Aerobee launch and $450,000 for each Viking launch. A series of seven ship-launched tests conducted by a University of Iowa team under James Van Allen achieved considerable success, with one flight grazing the edge of space with an apogee of Script error: No such module "convert"..[4]Template:Rp
Spacecraft development
US Air Force
Progress remained slow throughout 1952 on the Atlas, the nation's first intercontinental ballistic missile (ICBM), the contract for which had been awarded to Consolidated Vultee in January 1951 by the US Air Force's Air Research and Development Command. Conservative development policies and daunting technical problems were the official causes, but the Air Force's apparent lack of enthusiasm for the project, along with a limited budget and resources, were factors as well. It was not until the first successful H-bomb test at Elugelab in November 1952 that development of the Atlas, potentially capable of delivering such a weapon, garnered more support.[5]Template:Rp
US Army
On 8 April 1952, Redstone Arsenal in Alabama officially gave the name of "Redstone" to the surface-to-surface missile, capable of delivering nuclear or conventional warheads to a range of Script error: No such module "convert"., which they had started developing on 10 July 1951. The office of the Chief of Ordnance of the Army (OCO) tasked Chrysler Corporation to proceed with active work as the prime contractor on the missile by a letter order contract in October 1952; this contract definitized on 19 June 1953.[6]
Soviet military
In 1952, the Soviet Union focused its strategic rocket development on the R-5 missile, which superseded the overambitious Script error: No such module "convert". range R-3, previously canceled on 20 October 1951.[7]Template:Rp OKB-1 under Sergei Korolev completed the conceptual design for the R-5, able to carry the same Script error: No such module "convert". payload as the R-1 and R-2 but over a distance of Script error: No such module "convert".,[7]Template:Rp by 30 October 1951.[8]Template:Rp
This dramatic increase in performance of the R-5 over its predecessors was made possible through development of the RD-103 engine, an evolution of the RD-101 used in the R-2 missile, and by reducing the weight of the rocket through use of integrated tankage (while at the same time increasing propellant load by 60% over the R-2). The military had much more confidence in this incremental design than the radical leap forward that was the R-3, and work proceeded apace. Other innovations over the R-1 and R-2 included small aerodynamic rudders run by servomotors to replace the big fins of the R-1/R-2, and longitudinal acceleration integrators to improve the precision of engine cutoff and thus accuracy.[8]Template:Rp Two of the first ten R-5s produced underwent stand tests through February 1952,[9] and the sleek, cylindrical R-5, "the first Soviet strategic rocket", would be ready for its first launch March 1953.[8]Template:Rp
Also in 1952, the design bureau OKB-486, under Valentin Glushko, began developing the RD-105 and RD-106 engines for an even more powerful rocket: the five engine R-6 ICBM. Using an integrated solder-welded configuration, developed by engineer Aleksei Isaev, these LOX/kerosene engines would be more powerful single chamber engines than those used in earlier rockets. Four Script error: No such module "convert". RD-105 would power the R-6's four strap-on engines while a Script error: No such module "convert". RD-106 would power the central booster.[8]Template:Rp
That same year, there was also a series of fourteen test launches of the mass-produced version of R-2 missile, with a range of Script error: No such module "convert"..[7]Template:Rp Twelve of the missiles reached their targets.[7]Template:Rp The R-1 also was test-launched seven times.[10]
Civilian efforts
In October 1952, the General Assembly of the International Council of Scientific Unions (ICSU) adopted a proposal to undertake a third International Polar Year. This endeavor would involve both a wider scope, encompassing simultaneous observations of geophysical phenomena over the entire surface of the Earth including the Arctic and Antarctica, as well as a longer period, lasting 18 months. The International Geophysical Year (IGY), set for 1957–58, ultimately would involve the participation of 67 countries. To coordinate this massive effort, the ICSU formed the Template:Langx, which would hold four major meetings with representation from all participating countries over the next four years.[4]Template:Rp[11]Template:Rp
In 1951, the University of Maryland's Fred Singer gave a series of lectures to the British Interplanetary Society in London espousing the use of small artificial satellites to conduct scientific observations. In 1952 Singer expanded his audience through publications and public presentations on his proposals for "MOUSE" (Minimum Orbiting Unmanned Satellite of the Earth). Though dismissed by many as too radical and/or in conflict with human exploration of space, the proposal catalyzed serious discussion of the use of satellites for scientific research.[4]Template:Rp
Launches
| Template:Flatlist |
January
| Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
|---|---|---|---|---|---|---|---|
| Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
| Remarks | |||||||
| 30 January 20:45 |
Template:FlagiconAerobee RTV-A-1a | USAF 21 | Template:FlagiconHolloman LC-A | Template:FlagiconUS Air Force | |||
| Ionosphere 1 | AFCRC / University of Utah | Suborbital | Ionospheric | 30 January | Launch failure | ||
| Apogee: Script error: No such module "convert"., rocket exploded in tower[3]Template:Rp | |||||||
February
| Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
|---|---|---|---|---|---|---|---|
| Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
| Remarks | |||||||
| 19 February 14:49 |
Template:FlagiconAerobee RTV-A-1c | USAF 22 | Template:FlagiconHolloman LC-A | Template:FlagiconUS Air Force | |||
| AFCRC / University of Utah | Suborbital | Airglow | 19 February | Launch failure | |||
| Apogee: Script error: No such module "convert"., maiden (and only) flight of the RTV-A-1c, which was an unboosted version of the RTV-A-1a. There was a thrust chamber explosion in the tower, but the instrumentation was recovered intact.[3]Template:Rp | |||||||
| 19 February 17:00 |
Template:FlagiconAerobee RTV-N-10 | NRL 7 | Template:FlagiconWhite Sands LC-35 | Template:FlagiconUS Navy | |||
| NRL | Suborbital | Cosmic Radiation / Solar Radiation | 19 February | Successful | |||
| Apogee: Script error: No such module "convert".[3]Template:Rp | |||||||
| 29 February 14:40 |
Template:FlagiconAerobee RTV-A-1 | USAF 23 | Template:FlagiconHolloman LC-A | Template:FlagiconUS Air Force | |||
| AFCRC / University of Utah | Suborbital | Airglow | 29 February | Successful | |||
| Apogee: Script error: No such module "convert".[3]Template:Rp | |||||||
April
| Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
|---|---|---|---|---|---|---|---|
| Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
| Remarks | |||||||
| 22 April 17:28 |
Template:FlagiconAerobee RTV-A-1 | USAF 24 | Template:FlagiconHolloman LC-A | Template:FlagiconUS Air Force | |||
| AFCRC / Boston University | Suborbital | Ionospheric | 22 April | Successful | |||
| Apogee: Script error: No such module "convert".[3]Template:Rp | |||||||
| 30 April 13:30 |
Template:FlagiconAerobee RTV-N-10 | NRL 8 | Template:FlagiconWhite Sands LC-35 | Template:FlagiconUS Navy | |||
| NRL | Suborbital | Cosmic Radiation / Solar Radiation | 30 April | Successful | |||
| Apogee: Script error: No such module "convert".[3]Template:Rp | |||||||
May
| Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
|---|---|---|---|---|---|---|---|
| Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
| Remarks | |||||||
| 1 May 14:59 |
Template:FlagiconAerobee RTV-N-10 | NRL 9 | Template:FlagiconWhite Sands LC-35 | Template:FlagiconUS Navy | |||
| NRL | Suborbital | Cosmic Radiation / Solar Radiation | 1 May | Successful | |||
| Apogee: Script error: No such module "convert".[3]Template:Rp | |||||||
| 1 May 15:42 |
Template:FlagiconAerobee RTV-A-1 | USAF 25 | Template:FlagiconHolloman LC-A | Template:FlagiconUS Air Force | |||
| AFCRC / University of Rhode Island | Suborbital | Solar UV | 1 May | Successful | |||
| Apogee: Script error: No such module "convert".[3]Template:Rp | |||||||
| 5 May 13:44 |
Template:FlagiconAerobee RTV-N-10 | NRL 10 | Template:FlagiconWhite Sands LC-35 | Template:FlagiconUS Navy | |||
| NRL | Suborbital | Cosmic Radiation / Solar Radiation | 5 May | Successful | |||
| Apogee: Script error: No such module "convert".[3]Template:Rp | |||||||
| 15 May 01:15 |
Template:FlagiconAerobee XASR-SC-1 | SC 23 | Template:FlagiconWhite Sands LC-35 | Template:FlagiconUS Army | |||
| Template:FlagiconSphere | SCEL / University of Michigan | Suborbital | Aeronomy | 15 May | Successful | ||
| Apogee: Script error: No such module "convert".[3]Template:Rp | |||||||
| 20 May 02:07 |
Template:FlagiconAerobee XASR-SC-1 | SC 24 | Template:FlagiconWhite Sands LC-35 | Template:FlagiconUS Army | |||
| Template:FlagiconGrenades | USASC | Suborbital | Aeronomy | 20 May | Successful | ||
| Apogee: Script error: No such module "convert".[3]Template:Rp | |||||||
| 20 May 16:06 |
Template:FlagiconV-2 | V-2 No. 59 / TF-2 | Template:FlagiconWhite Sands LC-33 | Template:FlagiconUS Army | |||
| SCEL / University of Michigan | Suborbital | Aeronomy / Photography | 20 May | Successful | |||
| Apogee: Script error: No such module "convert".[3]Template:Rp | |||||||
| 21 May 15:15 |
Template:FlagiconAerobee RTV-A-1 | USAF 26 | Template:FlagiconHolloman LC-A | Template:FlagiconUS Air Force | |||
| Template:FlagiconAeromed 3 | AFCRL / WADC Aero-Medical Laboratory | Suborbital | Biological | 21 May | Successful | ||
| Carried 2 Philippine monkeys, Pat and Mike, and 2 mice; all recovered. Apogee: Script error: No such module "convert".[3]Template:Rp Flight tested requirement of restraints: one mouse was given a shelf to cling to; the other bounced from side to side of its smooth-sided plastic compartment. Acceleration was 15 gees for <1 second and 3-4 gees for 35 seconds. The two monkeys were strapped to their seats and anaesthetized. Mission demonstrated that pilot injury in rocket flight could be avoided with appropriate seats and straps.[12] | |||||||
June
| Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
|---|---|---|---|---|---|---|---|
| Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
| Remarks | |||||||
| 6 June 17:30 |
Template:FlagiconViking (second model) | Template:FlagiconWhite Sands LC-33 | Template:FlagiconUS Navy | ||||
| Template:FlagiconViking 8 | NRL | Suborbital | Accidental launch | 6 June | Launch failure | ||
| Apogee: Script error: No such module "convert"., accidentally launched during static fire ground test[13] | |||||||
| 18 June 17:50 |
Template:FlagiconAerobee RTV-A-1 | USAF 27 | Template:FlagiconHolloman LC-A | Template:FlagiconUS Air Force | |||
| AFCRC / University of Denver | Suborbital | Solar UV | 18 June | Successful | |||
| Apogee: Script error: No such module "convert".[3]Template:Rp | |||||||
| 30 June 14:32 |
Template:FlagiconAerobee RTV-A-1 | USAF 28 | Template:FlagiconHolloman LC-A | Template:FlagiconUS Air Force | |||
| Template:FlagiconAirglow 1 | AFCRC | Suborbital | Sky Brightness | 30 June | Successful | ||
| Apogee: Script error: No such module "convert".[3]Template:Rp | |||||||
August
| Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
|---|---|---|---|---|---|---|---|
| Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
| Remarks | |||||||
| 8 August | Template:FlagiconR-2 | Template:FlagiconKapustin Yar | Template:FlagiconOKB-1 | ||||
| OKB-1 | Suborbital | Missile test | 8 August | ||||
| First of fourteen test launches of mass-produced version; twelve reached their target[14][7]Template:Rp | |||||||
| August | Template:FlagiconR-2 | Template:FlagiconKapustin Yar | Template:FlagiconOKB-1 | ||||
| OKB-1 | Suborbital | Missile test | Same day | ||||
| Second of fourteen test launches of mass-produced version; twelve reached their target[14][7]Template:Rp | |||||||
| August | Template:FlagiconR-2 | Template:FlagiconKapustin Yar | Template:FlagiconOKB-1 | ||||
| OKB-1 | Suborbital | Missile test | Same day | ||||
| Third of fourteen test launches of mass-produced version; twelve reached their target[14][7]Template:Rp | |||||||
| August | Template:FlagiconR-2 | Template:FlagiconKapustin Yar | Template:FlagiconOKB-1 | ||||
| OKB-1 | Suborbital | Missile test | Same day | ||||
| Fourth of fourteen test launches of mass-produced version; twelve reached their target[14][7]Template:Rp | |||||||
| August | Template:FlagiconR-2 | Template:FlagiconKapustin Yar | Template:FlagiconOKB-1 | ||||
| OKB-1 | Suborbital | Missile test | Same day | ||||
| Fifth of fourteen test launches of mass-produced version; twelve reached their target[14][7]Template:Rp | |||||||
| August | Template:FlagiconR-2 | Template:FlagiconKapustin Yar | Template:FlagiconOKB-1 | ||||
| OKB-1 | Suborbital | Missile test | Same day | ||||
| Sixth of fourteen test launches of mass-produced version; twelve reached their target[14][7]Template:Rp | |||||||
| August | Template:FlagiconR-2 | Template:FlagiconKapustin Yar | Template:FlagiconOKB-1 | ||||
| OKB-1 | Suborbital | Missile test | Same day | ||||
| Seventh of fourteen test launches of mass-produced version; twelve reached their target[14][7]Template:Rp | |||||||
| August | Template:FlagiconR-2 | Template:FlagiconKapustin Yar | Template:FlagiconOKB-1 | ||||
| OKB-1 | Suborbital | Missile test | Same day | ||||
| Eighth of fourteen test launches of mass-produced version; twelve reached their target[14][7]Template:Rp | |||||||
| 20 August | Template:FlagiconR-1 | Template:FlagiconKapustin Yar | Template:FlagiconOKB-1 | ||||
| OKB-1 | Suborbital | Missile test | 20 August | Successful[10] | |||
| 21 August | Template:FlagiconR-1 | Template:FlagiconKapustin Yar | Template:FlagiconOKB-1 | ||||
| OKB-1 | Suborbital | Missile test | 21 August | Successful[10] | |||
| 21 August 06:25 |
Template:FlagiconDeacon rockoon | SUI 1 | Template:FlagiconScript error: No such module "WPSHIPS utilities"., Kane Basin | Template:FlagiconUS Coast Guard | |||
| University of Iowa | Suborbital | Cosmic Radiation | 21 August | Partial failure | |||
| Maiden flight of the Deacon Rockoon, (balloon) apogee: Script error: No such module "convert"., rocket failed to fire[3]Template:Rp | |||||||
| 22 August 07:33 |
Template:FlagiconV-2 | TF-3 | Template:FlagiconWhite Sands LC-33 | Template:FlagiconUS Army | |||
| NRL / AFCRC / National Institutes of Health | Suborbital | Aeronomy / Cosmic Radiation / Solar X-Ray / Magnetic Field / Sky Brightness | 22 August | Successful | |||
| Apogee: Script error: No such module "convert".[3]Template:Rp | |||||||
| 24 August 03:34 |
Template:FlagiconDeacon rockoon | SUI 2 | Template:FlagiconUSCGC Eastwind, northern Baffin Bay | Template:FlagiconUS Coast Guard | |||
| University of Iowa | Suborbital | Cosmic Radiation | 24 August | Partial failure | |||
| (Balloon) Apogee: Script error: No such module "convert".,[3]Template:Rp rocket failed to fire, but instrument package worked[4]Template:Rp | |||||||
| 25 August | Template:FlagiconR-1 | Template:FlagiconKapustin Yar | Template:FlagiconOKB-1 | ||||
| OKB-1 | Suborbital | Missile test | 25 August | Successful[10] | |||
| 26 August 18:53 |
Template:FlagiconAerobee RTV-A-1a | USAF 29 | Template:FlagiconHolloman LC-A | Template:FlagiconUS Air Force | |||
| Template:FlagiconIonosphere 2 | AFCRC / University of Utah | Suborbital | Ionospheric | 26 August | Launch failure | ||
| Apogee: Script error: No such module "convert".[3]Template:Rp | |||||||
| 29 August 00:26 |
Template:FlagiconDeacon rockoon | SUI 3 | Template:FlagiconUSCGC Eastwind, northern Baffin Bay | Template:FlagiconUS Coast Guard | |||
| University of Iowa | Suborbital | Cosmic Radiation | 29 August | Spacecraft failure | |||
| Apogee: Script error: No such module "convert".,[3]Template:Rp first successful firing of balloon-launched rocket, instruments failed to return data[4]Template:Rp | |||||||
| 29 August 07:36 |
Template:FlagiconDeacon rockoon | SUI 4 | Template:FlagiconUSCGC Eastwind, northern Baffin Bay | Template:FlagiconUS Coast Guard | |||
| University of Iowa | Suborbital | Cosmic Radiation | 29 August | Successful | |||
| Apogee: Script error: No such module "convert".[3]Template:Rp | |||||||
| 29 August 18:15 |
Template:FlagiconDeacon rockoon | SUI 5 | Template:FlagiconUSCGC Eastwind, northern Baffin Bay | Template:FlagiconUS Coast Guard | |||
| University of Iowa | Suborbital | Cosmic Radiation | 29 August | Successful | |||
| Apogee: Script error: No such module "convert".[3]Template:Rp | |||||||
| 31 August 21:10 |
Template:FlagiconDeacon rockoon | SUI 6 | Template:FlagiconUSCGC Eastwind, northern Baffin Bay | Template:FlagiconUS Coast Guard | |||
| University of Iowa | Suborbital | Cosmic Radiation | 31 August | Successful | |||
| Apogee: Script error: No such module "convert".[3]Template:Rp | |||||||
September
| Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
|---|---|---|---|---|---|---|---|
| Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
| Remarks | |||||||
| September | Template:FlagiconR-2 | Template:FlagiconKapustin Yar | Template:FlagiconOKB-1 | ||||
| OKB-1 | Suborbital | Missile test | Same day | ||||
| Ninth of fourteen test launches of mass-produced version; twelve reached their target[14][7]Template:Rp | |||||||
| September | Template:FlagiconR-2 | Template:FlagiconKapustin Yar | Template:FlagiconOKB-1 | ||||
| OKB-1 | Suborbital | Missile test | Same day | ||||
| Tenth of fourteen test launches of mass-produced version; twelve reached their target[14][7]Template:Rp | |||||||
| September | Template:FlagiconR-2 | Template:FlagiconKapustin Yar | Template:FlagiconOKB-1 | ||||
| OKB-1 | Suborbital | Missile test | Same day | ||||
| Eleventh of fourteen test launches of mass-produced version; twelve reached their target[14][7]Template:Rp | |||||||
| September | Template:FlagiconR-2 | Template:FlagiconKapustin Yar | Template:FlagiconOKB-1 | ||||
| OKB-1 | Suborbital | Missile test | Same day | ||||
| Twelfth of fourteen test launches of mass-produced version; twelve reached their target[14][7]Template:Rp | |||||||
| September | Template:FlagiconR-2 | Template:FlagiconKapustin Yar | Template:FlagiconOKB-1 | ||||
| OKB-1 | Suborbital | Missile test | Same day | ||||
| Thirteenth of fourteen test launches of mass-produced version; twelve reached their target[14][7]Template:Rp | |||||||
| 3 September 14:49 |
Template:FlagiconAerobee RTV-N-10 | NRL 11 | Template:FlagiconWhite Sands LC-35 | Template:FlagiconUS Navy | |||
| NRL | Suborbital | Solar Radiation | 3 September | Successful | |||
| Apogee: Script error: No such module "convert".[3]Template:Rp | |||||||
| 4 September 09:17 |
Template:FlagiconDeacon rockoon | SUI 7 | Template:FlagiconScript error: No such module "WPSHIPS utilities"., northern Baffin Bay | Template:FlagiconUS Coast Guard | |||
| University of Iowa | Suborbital | Cosmic Radiation | 4 September | Successful | |||
| Apogee: Script error: No such module "convert".[3]Template:Rp | |||||||
| 18 September | Template:FlagiconR-2 | Template:FlagiconKapustin Yar | Template:FlagiconOKB-1 | ||||
| OKB-1 | Suborbital | Missile test | 18 September | ||||
| Last of fourteen test launches of mass-produced version; twelve reached their target[14][7]Template:Rp | |||||||
| 19 September 15:49 |
Template:FlagiconV-2 | TF-5 | Template:FlagiconWhite Sands LC-33 | Template:FlagiconUS Army | |||
| SCEL / University of Michigan | Suborbital | Aeronomy | 19 September | Launch failure | |||
| Final flight of the V-2, apogee: Script error: No such module "convert"., tail exploded at 27 seconds[3]Template:Rp | |||||||
| 25 September 03:50 |
Template:FlagiconAerobee XASR-SC-1 | SC 25 | Template:FlagiconWhite Sands LC-35 | Template:FlagiconUS Army | |||
| Template:FlagiconGrenades | SCEL | Suborbital | Aeronomy | 25 September | Successful | ||
| Apogee: Script error: No such module "convert".[3]Template:Rp | |||||||
October
| Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
|---|---|---|---|---|---|---|---|
| Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
| Remarks | |||||||
| 10 October 14:24 |
Template:FlagiconAerobee RTV-A-1 | USAF 30 | Template:FlagiconHolloman LC-A | Template:FlagiconUS Air Force | |||
| AFCRC / University of Denver | Suborbital | Solar UV | 10 October | Successful | |||
| Apogee: Script error: No such module "convert".[3]Template:Rp | |||||||
| 22 October 14:35 |
Template:FlagiconAerobee RTV-A-1 | USAF 31 | Template:FlagiconHolloman LC-A | Template:FlagiconUS Air Force | |||
| AFCRC / University of Michigan | Suborbital | Aeronomy | 22 October | Successful | |||
| Apogee: Script error: No such module "convert".[3]Template:Rp | |||||||
| 23 October 03:45 |
Template:FlagiconAerobee XASR-SC-2 | SC 26 | Template:FlagiconWhite Sands LC-35 | Template:FlagiconUS Army | |||
| Template:FlagiconGrenades | SCEL | Suborbital | Aeronomy | 23 October | Successful | ||
| Apogee: Script error: No such module "convert".[3]Template:Rp | |||||||
| 29 October | Template:FlagiconR-1 | Template:FlagiconKapustin Yar | Template:FlagiconOKB-1 | ||||
| OKB-1 | Suborbital | Missile test | 29 October | Successful[10] | |||
| 30 October | Template:FlagiconR-1 | Template:FlagiconKapustin Yar | Template:FlagiconOKB-1 | ||||
| OKB-1 | Suborbital | Missile test | 30 October | Successful[10] | |||
| 30 October | Template:FlagiconR-1 | Template:FlagiconKapustin Yar | Template:FlagiconOKB-1 | ||||
| OKB-1 | Suborbital | Missile test | 30 October | Successful[10] | |||
November
| Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
|---|---|---|---|---|---|---|---|
| Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
| Remarks | |||||||
| 6 November 15:56 |
Template:FlagiconAerobee RTV-A-1 | USAF 32 | Template:FlagiconHolloman LC-A | Template:FlagiconUS Air Force | |||
| Airglow 2 | AFCRC | Suborbital | Sky Brightness | 6 November | Successful | ||
| Apogee: Script error: No such module "convert".[3]Template:Rp | |||||||
| 21 November | Template:FlagiconR-1 | Template:FlagiconKapustin Yar | Template:FlagiconOKB-1 | ||||
| OKB-1 | Suborbital | Missile test | 21 November | Successful[10] | |||
December
| Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
|---|---|---|---|---|---|---|---|
| Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
| Remarks | |||||||
| 11 December 23:47 |
Template:FlagiconAerobee XASR-SC-1 | SC 29 | Template:FlagiconWhite Sands LC-35 | Template:FlagiconUS Army | |||
| Template:FlagiconSphere | SCEL / University of Michigan | Suborbital | Aeronomy / Cosmic Radiation | 11 December | Successful | ||
| Apogee: Script error: No such module "convert".[3]Template:Rp | |||||||
| 12 December 19:38 |
Template:FlagiconAerobee RTV-A-1 | USAF 33 | Template:FlagiconHolloman LC-A | Template:FlagiconUS Air Force | |||
| AFCRC / University of Colorado | Suborbital | Solar UV | 12 December | Successful | |||
| Final flight of the RTV-A-1, apogee: Script error: No such module "convert".[3]Template:Rp | |||||||
| 15 December 21:38 |
Template:FlagiconViking (second model) | Template:FlagiconWhite Sands LC-33 | Template:FlagiconUS Navy | ||||
| Template:FlagiconViking 9 | NRL | Suborbital | Solar Radiation / Cosmic Radiation / Photography | 15 December | Successful | ||
| Apogee: Script error: No such module "convert".[3]Template:Rp | |||||||
| Template:Flatlist |
Suborbital launch statistics
By country
| Country | Launches | Successes | Failures | Partial failures | |
|---|---|---|---|---|---|
| Template:Flagcountry | 21 | 19 | 0 | 2 | |
| Template:Flagcountry | 35 | 27 | 5 | 3 | |
| World | Script error: No such module "math". | Script error: No such module "math". | Script error: No such module "math". | Script error: No such module "math". | |
By rocket
Script error: No such module "Chart".
| Rocket | Country | Launches | Successes | Failures | Partial failures |
Remarks |
|---|---|---|---|---|---|---|
| V-2 | Template:Flagcountry | 3 | 2 | 1 | 0 | Retired |
| Viking (second model) | Template:Flagcountry | 2 | 1 | 1 | 0 | Maiden flight |
| Aerobee RTV-N-10 | Template:Flagcountry | 5 | 5 | 0 | 0 | |
| Aerobee XASR-SC-1 | Template:Flagcountry | 4 | 4 | 0 | 0 | |
| Aerobee XASR-SC-2 | Template:Flagcountry | 1 | 1 | 0 | 0 | |
| Aerobee RTV-A-1 | Template:Flagcountry | 10 | 10 | 0 | 0 | Retired |
| Aerobee RTV-A-1a | Template:Flagcountry | 2 | 0 | 2 | 0 | |
| Aerobee RTV-A-1c | Template:Flagcountry | 1 | 0 | 1 | 0 | Maiden flight, retired |
| Deacon rockoon | Template:Flagcountry | 7 | 4 | 0 | 3 | Maiden flight |
| R-1 | Template:Flagcountry | 7 | 7 | 0 | 0 | |
| R-2 | Template:Flagcountry | 14 | 12 | 0 | 2 |
See also
References
<templatestyles src="Reflist/styles.css" />
- ↑ Script error: No such module "Citation/CS1".
- ↑ a b c Script error: No such module "citation/CS1".
- ↑ a b c d e f g h i j k l m n o p q r s t u v w x y z aa ab ac ad ae af ag ah ai Script error: No such module "citation/CS1".
- ↑ a b c d e Script error: No such module "citation/CS1".
- ↑ Script error: No such module "citation/CS1".
- ↑ Script error: No such module "citation/CS1".
- ↑ a b c d e f g h i j k l m n o p q r Script error: No such module "citation/CS1".
- ↑ a b c d Script error: No such module "citation/CS1".
- ↑ Script error: No such module "citation/CS1".
- ↑ a b c d e f g h Script error: No such module "citation/CS1".
- ↑ Script error: No such module "citation/CS1".
- ↑ Script error: No such module "citation/CS1".
- ↑ Script error: No such module "citation/CS1".
- ↑ a b c d e f g h i j k l m n Script error: No such module "citation/CS1".
Script error: No such module "Check for unknown parameters".
Script error: No such module "Navbox".