Rockets | |
---|---|
Maiden flights | Aerobee RTV-A-1c Viking (second model) Deacon rockoon |
Retirements | V-2 Aerobee RTV-A-1 Aerobee RTV-A-1c |
In 1952, several branches of the United States' military, often in partnership with civilian organizations, continued their programs of sounding rocket research beyond the 100 kilometres (62 mi) 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 135 mi (217 km), 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.
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] : 172–173
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 4 to 5 miles (6 to 8 km) downrange to the southeast. [2] : 180–181
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 135 miles (217 km), 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] : 185–203
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 7.1 kilometres (4.4 mi) before its tail exploded 27 seconds into the flight. [3] : 469–470
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 55 miles (89 km). [4] : 10–18
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] : 59–71
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 200 miles (320 km), 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]
In 1952, the Soviet Union focused its strategic rocket development on the R-5 missile, which superseded the overambitious 3,000 kilometres (1,900 mi) range R-3, previously canceled on 20 October 1951. [7] : 275–6 OKB-1 under Sergei Korolev completed the conceptual design for the R-5, able to carry the same 1,000 kilograms (2,200 lb) payload as the R-1 and R-2 but over a distance of 1,200 kilometres (750 mi), [7] : 242 by 30 October 1951. [8] : 97
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] : 99–100 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] : 99–100
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 539.37 kN (121,260 lbf) RD-105 would power the R-6's four strap-on engines while a 519.75 kN (116,840 lbf) RD-106 would power the central booster. [8] : 108–109
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 600 kilometres (370 mi). [7] : 48–9 Twelve of the missiles reached their targets. [7] : 266 The R-1 also was test-launched seven times. [10]
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 Comité Speciale de l'Année Géophysique Internationale (CSAGI), 'International Geophysical Year Special Committee', which would hold four major meetings with representation from all participating countries over the next four years. [4] : 69 [11] : 19–21
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] : 73
Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
---|---|---|---|---|---|---|---|
Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
Remarks | |||||||
30 January 20:45 | Aerobee RTV-A-1a | USAF 21 | Holloman LC-A | US Air Force | |||
Ionosphere 1 | AFCRC / University of Utah | Suborbital | Ionospheric | 30 January | Launch failure | ||
Apogee: 0 kilometres (0 mi), rocket exploded in tower [3] : 85 |
Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
---|---|---|---|---|---|---|---|
Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
Remarks | |||||||
19 February 14:49 | Aerobee RTV-A-1c | USAF 22 | Holloman LC-A | US Air Force | |||
AFCRC / University of Utah | Suborbital | Airglow | 19 February | Launch failure | |||
Apogee: 0 kilometres (0 mi), 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] : 86 | |||||||
19 February 17:00 | Aerobee RTV-N-10 | NRL 7 | White Sands LC-35 | US Navy | |||
NRL | Suborbital | Cosmic Radiation / Solar Radiation | 19 February | Successful | |||
Apogee: 81.3 kilometres (50.5 mi) [3] : 303–304 | |||||||
29 February 14:40 | Aerobee RTV-A-1 | USAF 23 | Holloman LC-A | US Air Force | |||
AFCRC / University of Utah | Suborbital | Airglow | 29 February | Successful | |||
Apogee: 89.3 kilometres (55.5 mi) [3] : 87–88 |
Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
---|---|---|---|---|---|---|---|
Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
Remarks | |||||||
22 April 17:28 | Aerobee RTV-A-1 | USAF 24 | Holloman LC-A | US Air Force | |||
AFCRC / Boston University | Suborbital | Ionospheric | 22 April | Successful | |||
Apogee: 113 kilometres (70 mi) [3] : 89–90 | |||||||
30 April 13:30 | Aerobee RTV-N-10 | NRL 8 | White Sands LC-35 | US Navy | |||
NRL | Suborbital | Cosmic Radiation / Solar Radiation | 30 April | Successful | |||
Apogee: 127.8 kilometres (79.4 mi) [3] : 305 |
Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
---|---|---|---|---|---|---|---|
Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
Remarks | |||||||
1 May 14:59 | Aerobee RTV-N-10 | NRL 9 | White Sands LC-35 | US Navy | |||
NRL | Suborbital | Cosmic Radiation / Solar Radiation | 1 May | Successful | |||
Apogee: 126.0 kilometres (78.3 mi) [3] : 305 | |||||||
1 May 15:42 | Aerobee RTV-A-1 | USAF 25 | Holloman LC-A | US Air Force | |||
AFCRC / University of Rhode Island | Suborbital | Solar UV | 1 May | Successful | |||
Apogee: 91 kilometres (57 mi) [3] : 91–92 | |||||||
5 May 13:44 | Aerobee RTV-N-10 | NRL 10 | White Sands LC-35 | US Navy | |||
NRL | Suborbital | Cosmic Radiation / Solar Radiation | 5 May | Successful | |||
Apogee: 127.0 kilometres (78.9 mi) [3] : 305 | |||||||
15 May 01:15 | Aerobee XASR-SC-1 | SC 23 | White Sands LC-35 | US Army | |||
Sphere | SCEL / University of Michigan | Suborbital | Aeronomy | 15 May | Successful | ||
Apogee: 76.1 kilometres (47.3 mi) [3] : 233–234 | |||||||
20 May 02:07 | Aerobee XASR-SC-1 | SC 24 | White Sands LC-35 | US Army | |||
Grenades | USASC | Suborbital | Aeronomy | 20 May | Successful | ||
Apogee: 89.5 kilometres (55.6 mi) [3] : 235–236 | |||||||
20 May 16:06 | V-2 | V-2 No. 59 / TF-2 | White Sands LC-33 | US Army | |||
SCEL / University of Michigan | Suborbital | Aeronomy / Photography | 20 May | Successful | |||
Apogee: 103.5 kilometres (64.3 mi) [3] : 455–456, 464 | |||||||
21 May 15:15 | Aerobee RTV-A-1 | USAF 26 | Holloman LC-A | US Air Force | |||
Aeromed 3 | AFCRL / WADC Aero-Medical Laboratory | Suborbital | Biological | 21 May | Successful | ||
Carried 2 Philippine monkeys, Pat and Mike, and 2 mice; all recovered. Apogee: 61 kilometres (38 mi) [3] : 93–94 |
Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
---|---|---|---|---|---|---|---|
Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
Remarks | |||||||
6 June 17:30 | Viking (second model) | White Sands LC-33 | US Navy | ||||
Viking 8 | NRL | Suborbital | Accidental launch | 6 June | Launch failure | ||
Apogee: 6 kilometres (3.7 mi), accidentally launched during static fire ground test [12] | |||||||
18 June 17:50 | Aerobee RTV-A-1 | USAF 27 | Holloman LC-A | US Air Force | |||
AFCRC / University of Denver | Suborbital | Solar UV | 18 June | Successful | |||
Apogee: 105 kilometres (65 mi) [3] : 95–96 | |||||||
30 June 14:32 | Aerobee RTV-A-1 | USAF 28 | Holloman LC-A | US Air Force | |||
Airglow 1 | AFCRC | Suborbital | Sky Brightness | 30 June | Successful | ||
Apogee: 101 kilometres (63 mi) [3] : 97–98 |
Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
---|---|---|---|---|---|---|---|
Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
Remarks | |||||||
8 August | R-2 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | 8 August | ||||
First of fourteen test launches of mass-produced version; twelve reached their target [13] [7] : 266 | |||||||
August | R-2 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | Same day | ||||
Second of fourteen test launches of mass-produced version; twelve reached their target [13] [7] : 266 | |||||||
August | R-2 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | Same day | ||||
Third of fourteen test launches of mass-produced version; twelve reached their target [13] [7] : 266 | |||||||
August | R-2 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | Same day | ||||
Fourth of fourteen test launches of mass-produced version; twelve reached their target [13] [7] : 266 | |||||||
August | R-2 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | Same day | ||||
Fifth of fourteen test launches of mass-produced version; twelve reached their target [13] [7] : 266 | |||||||
August | R-2 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | Same day | ||||
Sixth of fourteen test launches of mass-produced version; twelve reached their target [13] [7] : 266 | |||||||
August | R-2 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | Same day | ||||
Seventh of fourteen test launches of mass-produced version; twelve reached their target [13] [7] : 266 | |||||||
August | R-2 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | Same day | ||||
Eighth of fourteen test launches of mass-produced version; twelve reached their target [13] [7] : 266 | |||||||
20 August | R-1 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | 20 August | Successful [10] | |||
21 August | R-1 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | 21 August | Successful [10] | |||
21 August 06:25 | Deacon rockoon | SUI 1 | USCGC Eastwind, Kane Basin | US Coast Guard | |||
University of Iowa | Suborbital | Cosmic Radiation | 21 August | Partial failure | |||
Maiden flight of the Deacon Rockoon, (balloon) apogee: 21.4 kilometres (13.3 mi), rocket failed to fire [3] : 312 | |||||||
22 August 07:33 | V-2 | TF-3 | White Sands LC-33 | US Army | |||
NRL / AFCRC / National Institutes of Health | Suborbital | Aeronomy / Cosmic Radiation / Solar X-Ray / Magnetic Field / Sky Brightness | 22 August | Successful | |||
Apogee: 78.1 kilometres (48.5 mi) [3] : 465–466 | |||||||
24 August 03:34 | Deacon rockoon | SUI 2 | USCGC Eastwind, northern Baffin Bay | US Coast Guard | |||
University of Iowa | Suborbital | Cosmic Radiation | 24 August | Partial failure | |||
(Balloon) Apogee: 21.4 kilometres (13.3 mi), [3] : 312 rocket failed to fire, but instrument package worked [4] : 17 | |||||||
25 August | R-1 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | 25 August | Successful [10] | |||
26 August 18:53 | Aerobee RTV-A-1a | USAF 29 | Holloman LC-A | US Air Force | |||
Ionosphere 2 | AFCRC / University of Utah | Suborbital | Ionospheric | 26 August | Launch failure | ||
Apogee: 32 kilometres (20 mi) [3] : 99–100 | |||||||
29 August 00:26 | Deacon rockoon | SUI 3 | USCGC Eastwind, northern Baffin Bay | US Coast Guard | |||
University of Iowa | Suborbital | Cosmic Radiation | 29 August | Spacecraft failure | |||
Apogee: 61.0 kilometres (37.9 mi), [3] : 312 first successful firing of balloon-launched rocket, instruments failed to return data [4] : 18 | |||||||
29 August 07:36 | Deacon rockoon | SUI 4 | USCGC Eastwind, northern Baffin Bay | US Coast Guard | |||
University of Iowa | Suborbital | Cosmic Radiation | 29 August | Successful | |||
Apogee: 59.4 kilometres (36.9 mi) [3] : 312 | |||||||
29 August 18:15 | Deacon rockoon | SUI 5 | USCGC Eastwind, northern Baffin Bay | US Coast Guard | |||
University of Iowa | Suborbital | Cosmic Radiation | 29 August | Successful | |||
Apogee: 76.1 kilometres (47.3 mi) [3] : 312 | |||||||
31 August 21:10 | Deacon rockoon | SUI 6 | USCGC Eastwind, northern Baffin Bay | US Coast Guard | |||
University of Iowa | Suborbital | Cosmic Radiation | 31 August | Successful | |||
Apogee: 64.1 kilometres (39.8 mi) [3] : 313 |
Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
---|---|---|---|---|---|---|---|
Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
Remarks | |||||||
September | R-2 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | Same day | ||||
Ninth of fourteen test launches of mass-produced version; twelve reached their target [13] [7] : 266 | |||||||
September | R-2 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | Same day | ||||
Tenth of fourteen test launches of mass-produced version; twelve reached their target [13] [7] : 266 | |||||||
September | R-2 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | Same day | ||||
Eleventh of fourteen test launches of mass-produced version; twelve reached their target [13] [7] : 266 | |||||||
September | R-2 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | Same day | ||||
Twelfth of fourteen test launches of mass-produced version; twelve reached their target [13] [7] : 266 | |||||||
September | R-2 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | Same day | ||||
Thirteenth of fourteen test launches of mass-produced version; twelve reached their target [13] [7] : 266 | |||||||
3 September 14:49 | Aerobee RTV-N-10 | NRL 11 | White Sands LC-35 | US Navy | |||
NRL | Suborbital | Solar Radiation | 3 September | Successful | |||
Apogee: 99.0 kilometres (61.5 mi) [3] : 305 | |||||||
4 September 09:17 | Deacon rockoon | SUI 7 | USCGC Eastwind, northern Baffin Bay | US Coast Guard | |||
University of Iowa | Suborbital | Cosmic Radiation | 4 September | Successful | |||
Apogee: 64.1 kilometres (39.8 mi) [3] : 313 | |||||||
18 September | R-2 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | 18 September | ||||
Last of fourteen test launches of mass-produced version; twelve reached their target [13] [7] : 266 | |||||||
19 September 15:49 | V-2 | TF-5 | White Sands LC-33 | US Army | |||
SCEL / University of Michigan | Suborbital | Aeronomy | 19 September | Launch failure | |||
Final flight of the V-2, apogee: 7.1 kilometres (4.4 mi), tail exploded at 27 seconds [3] : 469–470 | |||||||
25 September 03:50 | Aerobee XASR-SC-1 | SC 25 | White Sands LC-35 | US Army | |||
Grenades | SCEL | Suborbital | Aeronomy | 25 September | Successful | ||
Apogee: 117 kilometres (73 mi) [3] : 239 |
Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
---|---|---|---|---|---|---|---|
Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
Remarks | |||||||
10 October 14:24 | Aerobee RTV-A-1 | USAF 30 | Holloman LC-A | US Air Force | |||
AFCRC / University of Denver | Suborbital | Solar UV | 10 October | Successful | |||
Apogee: 110 kilometres (68 mi) [3] : 102–103 | |||||||
22 October 14:35 | Aerobee RTV-A-1 | USAF 31 | Holloman LC-A | US Air Force | |||
AFCRC / University of Michigan | Suborbital | Aeronomy | 22 October | Successful | |||
Apogee: 100 kilometres (62 mi) [3] : 104–105 | |||||||
23 October 03:45 | Aerobee XASR-SC-2 | SC 26 | White Sands LC-35 | US Army | |||
Grenades | SCEL | Suborbital | Aeronomy | 23 October | Successful | ||
Apogee: 112.0 kilometres (69.6 mi) [3] : 237–238 | |||||||
29 October | R-1 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | 29 October | Successful [10] | |||
30 October | R-1 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | 30 October | Successful [10] | |||
30 October | R-1 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | 30 October | Successful [10] |
Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
---|---|---|---|---|---|---|---|
Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
Remarks | |||||||
6 November 15:56 | Aerobee RTV-A-1 | USAF 32 | Holloman LC-A | US Air Force | |||
Airglow 2 | AFCRC | Suborbital | Sky Brightness | 6 November | Successful | ||
Apogee: 76 kilometres (47 mi) [3] : 106–107 | |||||||
21 November | R-1 | Kapustin Yar | OKB-1 | ||||
OKB-1 | Suborbital | Missile test | 21 November | Successful [10] |
Date and time (UTC) | Rocket | Flight number | Launch site | LSP | |||
---|---|---|---|---|---|---|---|
Payload | Operator | Orbit | Function | Decay (UTC) | Outcome | ||
Remarks | |||||||
11 December 23:47 | Aerobee XASR-SC-1 | SC 29 | White Sands LC-35 | US Army | |||
Sphere | SCEL / University of Michigan | Suborbital | Aeronomy / Cosmic Radiation | 11 December | Successful | ||
Apogee: 105.1 kilometres (65.3 mi) [3] : 244–245 | |||||||
12 December 19:38 | Aerobee RTV-A-1 | USAF 33 | Holloman LC-A | US Air Force | |||
AFCRC / University of Colorado | Suborbital | Solar UV | 12 December | Successful | |||
Final flight of the RTV-A-1, apogee: 89 kilometres (55 mi) [3] : 108–109 | |||||||
15 December 21:38 | Viking (second model) | White Sands LC-33 | US Navy | ||||
Viking 9 | NRL | Suborbital | Solar Radiation / Cosmic Radiation / Photography | 15 December | Successful | ||
Apogee: 219 kilometres (136 mi) [3] : 494 |
Country | Launches | Successes | Failures | Partial failures | |
---|---|---|---|---|---|
United States | 35 | 27 | 5 | 3 | |
Soviet Union | 21 | 19 | 0 | 2 |
Rocket | Country | Launches | Successes | Failures | Partial failures | Remarks |
---|---|---|---|---|---|---|
V-2 | United States | 3 | 2 | 1 | 0 | Retired |
Viking (second model) | United States | 2 | 1 | 1 | 0 | Maiden flight |
Aerobee RTV-N-10 | United States | 5 | 5 | 0 | 0 | |
Aerobee XASR-SC-1 | United States | 4 | 4 | 0 | 0 | |
Aerobee XASR-SC-2 | United States | 1 | 1 | 0 | 0 | |
Aerobee RTV-A-1 | United States | 10 | 10 | 0 | 0 | Retired |
Aerobee RTV-A-1a | United States | 2 | 0 | 2 | 0 | |
Aerobee RTV-A-1c | United States | 1 | 0 | 1 | 0 | Maiden flight, retired |
Deacon rockoon | United States | 7 | 4 | 0 | 3 | Maiden flight |
R-1 | Soviet Union | 7 | 7 | 0 | 0 | |
R-2 | Soviet Union | 14 | 12 | 0 | 2 |
The Army Ballistic Missile Agency (ABMA) was formed to develop the U.S. Army's first large ballistic missile. The agency was established at Redstone Arsenal on 1 February 1956, and commanded by Major General John B. Medaris with Wernher von Braun as technical director.
The Aerobee rocket was one of the United States' most produced and productive sounding rockets. Developed by the Aerojet Corporation, the Aerobee was designed to combine the altitude and launching capability of the V-2 with the cost effectiveness and mass production of the WAC Corporal. More than 1000 Aerobees were launched between 1947 and 1985, returning vast amounts of astronomical, physical, aeronomical, and biomedical data.
James Alfred Van Allen was an American space physicist at the University of Iowa. He was instrumental in establishing the field of magnetospheric research in space.
A sounding rocket or rocketsonde, sometimes called a research rocket or a suborbital rocket, is an instrument-carrying rocket designed to take measurements and perform scientific experiments during its sub-orbital flight. The rockets are used to launch instruments from 48 to 145 km above the surface of the Earth, the altitude generally between weather balloons and satellites; the maximum altitude for balloons is about 40 km and the minimum for satellites is approximately 121 km. Certain sounding rockets have an apogee between 1,000 and 1,500 km, such as the Black Brant X and XII, which is the maximum apogee of their class. For certain purposes Sounding Rockets may be flown to altitudes as high as 3,000 kilometers to allow observing times of around 40 minutes to provide geophysical observations of the magnetosphere, ionosphere, thermosphere and mesosphere. Sounding rockets have been used for the examination of atmospheric nuclear tests by revealing the passage of the shock wave through the atmosphere. In more recent times Sounding Rockets have been used for other nuclear weapons research. Sounding rockets often use military surplus rocket motors. NASA routinely flies the Terrier Mk 70 boosted Improved Orion, lifting 270–450-kg (600–1,000-pound) payloads into the exoatmospheric region between 97 and 201 km.
The R-2 was a Soviet short-range ballistic missile developed from and having twice the range as the R-1 missile. Developed from 1946-1951, the R-2 entered service in numbers in 1953 and was deployed in mobile units throughout the Soviet Union until 1962. A sounding rocket derivative, the R-2A, tested a prototype of the dog-carrying capsule flown on Sputnik 2 in 1957. The same year, the R-2 was licensed for production in The People's Republic of China, where it entered service as the Dongfeng 1.
The PGM-19 Jupiter was the first nuclear armed, medium-range ballistic missile (MRBM) of the United States Air Force (USAF). It was a liquid-propellant rocket using RP-1 fuel and LOX oxidizer, with a single Rocketdyne LR79-NA rocket engine producing 667 kilonewtons (150,000 lbf) of thrust. It was armed with the 1.44 megatons of TNT (6.0 PJ) W49 nuclear warhead. The prime contractor was the Chrysler Corporation.
The Vanguard rocket was intended to be the first launch vehicle the United States would use to place a satellite into orbit. Instead, the Sputnik crisis caused by the surprise launch of Sputnik 1 led the U.S., after the failure of Vanguard TV-3, to quickly orbit the Explorer 1 satellite using a Juno I rocket, making Vanguard 1 the second successful U.S. orbital launch.
The Aerojet General X-8 was an unguided, spin-stabilized sounding rocket designed to launch a 150 lb (68 kg) payload to 200,000 feet (61.0 km). The X-8 was a version of the prolific Aerobee rocket family.
Viking was a series of twelve sounding rockets designed and built by the Glenn L. Martin Company under the direction of the U.S. Naval Research Laboratory (NRL). Designed to supersede the German V-2 as a research vehicle, the Viking was the most advanced large, liquid-fueled rocket developed in the United States in the late 1940s, providing much engineering experience while returning valuable scientific data from the edge of space between 1949 and 1955. Viking 4, launched in 1950, was the first sounding rocket to be launched from the deck of a ship.
A rockoon is a sounding rocket that, rather than being lit immediately while still on the ground, is first carried into the upper atmosphere by a gas-filled balloon, then separated from the balloon and ignited. This allows the rocket to achieve a higher altitude, as the rocket does not have to move under power through the lower and thicker layers of the atmosphere. A 2016 study by Acta Astronautica concluded that low-mass and high altitude launches give the best results.
The first orbital flight of an artificial satellite, Sputnik 1, was launched in October 1957, by the Soviet Union. In November, the second orbital flight took place. The Soviet Union launched the first animal to orbit the Earth, a dog, Laika, who died in orbit a few hours after launch.
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.
Project Hermes was a missile research program run by the Ordnance Corps of the United States Army from November 15, 1944, to December 31, 1954, in response to Germany's rocket attacks in Europe during World War II. The program was to determine the missile needs of army field forces. A research and development partnership between the Ordnance Corps and General Electric started November 20, 1944 and resulted in the "development of long-range missiles that could be used against both ground targets and high-altitude aircraft."
This is a list of spaceflight related events which occurred in 1956.
In 1955, both the United States and the Soviet Union (USSR) announced plans for launching the world's first satellites during the International Geophysical Year (IGY) of 1957–58. Project Vanguard, proposed by the US Navy, won out over the US Army's Project Orbiter as the satellite and rocket design to be flown in the IGY. Development of Intercontinental Ballistic Missiles, the Atlas by the US and the R-7 by the USSR, accelerated, entering the design and construction phase.
The year 1954 saw the conception of Project Orbiter, the first practicable satellite launching project, utilizing the Redstone, a newly developed Short Range Ballistic Missile.
The year 1951 saw extensive exploration of space by the United States and the Soviet Union (USSR) using suborbital rockets. The Soviets launched their first series of biomedical tests to the 100-kilometre (62 mi) boundary of space. Several American agencies launched more than a dozen scientific sounding rocket flights between them. The US Navy launched its Viking sounding rocket for the seventh time since 1949, this time to a record-breaking 136 miles (219 km) in August 1951.
Milton William Rosen was a United States Navy engineer and project manager in the US space program between the end of World War II and the early days of the Apollo Program. He led development of the Viking and Vanguard rockets, and was influential in the critical decisions early in NASA's history that led to the definition of the Saturn rockets, which were central to the eventual success of the American Moon landing program. He died of prostate cancer in 2014.
The year 1953 saw the rockoon join the stable of sounding rockets capable of reaching beyond the 100 kilometres (62 mi) boundary of space. Employed by both the University of Iowa and the Naval Research Laboratory, 22 total were launched from the decks of the USS Staten Island and the USCGC Eastwind this year. All branches of the United States military continued their program of Aerobee sounding rocket launches, a total of 23 were launched throughout 1953. The Soviet Union launched no sounding rockets in 1953; however, the Soviet Union did conduct several series of missile test launches.