1953 in spaceflight

The year 1953 saw the rockoon joining the Aerobee sounding rocket beyond the 100 kilometres (62 mi) boundary of space (as defined by the World Air Sports Federation),[1]. Both the United States and the Union of Soviet Socialist Republics continued their development of ballistic missiles, the United States Air Force with its Atlas ICBM, the United States Army with its Redstone SRBM, the Soviet OKB-1 with its R-5 IRBM, and Factory 586 with its R-12 IRBM.

1953 in spaceflight
Launch of a Deacon Rockoon, several such launches occurred in 1953
Rockets
Maiden flightsR-5 Pobeda
RetirementsAerobee RTV-A-1
Aerobee XASR-SC-1
Aerobee XASR-SC-2

Space exploration highlights

U.S. Navy

On 25 May, 1953, Viking 10, originally planned to be the last of the Naval Research Laboratory-built Viking rockets, arrived at White Sands Missile Range in New Mexico. A successful static firing on 18 June cleared the way for a 30 June launch date, a schedule that had been made months prior, before the rocket had even left the Glenn L. Martin Company plant where it had been built.

At the moment of liftoff, the tail of Viking 10 exploded, setting the rocket afire. Water was immediately flooded into the rocket's base in an attempt to extinguish the fire, but flames continued to burn in the East Quadrant of the firing platform. Half an hour after launch, two of the launch team under manager Milton Rosen were dispatched to put out the fire to salvage what remained of the rocket.

Their successful efforts were then threatened by a slow leak in the propellant tank. The vacuum created by the departing fuel was causing the tank to dimple with the danger of implosion that would cause the rocket to collapse. Lieutenant Joseph Pitts, a member of the launch team, shot a rifle round into the tank, equalizing the pressure and saving the rocket.

Three hours after the attempted launch, the last of the alcohol propellant had been drained from Viking 10. The launch team was able to salvage the instrument package of cameras, including X-ray detectors, cosmic ray emulsions, and a radio-frequency mass-spectrometer, valued at tens of thousands of dollars, although there was concern that the rocket was irreparable.

A thorough investigation of the explosion began in July, but a conclusive cause could not be determined. In a reported presented in September, Milton Rosen noted that a similar occurrence had not happened in more than 100 prior tests of the Viking motor. It was decided to rebuild Viking 10, and a program for closer monitoring of potential fail points was implemented for the next launch, scheduled for 1954.[2]

American civilian efforts

After the successful field tests of balloon-launched rockets (rockoons) the previous year, the University of Iowa physics team lead by Professor James Van Allen, embarked on a second rockoon expedition aboard the USS Staten Island in summer 1953 with improved equipment. The new Skyhook balloons increased the rocket firing altitude from 40,000 feet (12,000 m) to 50,000 feet (15,000 m) affording a peak rocket altitude of 57 miles (92 km). The total payload weights were increased by 2 pounds (0.91 kg) to 30 pounds (14 kg). Between 18 July and 5 September, the Iowa team launched 16 rockoons from a variety of latitudes, seven of which reached useful altitudes and returned usable data. An NRL team aboard the same vessel launched six rockoons, of which half were complete successes. Data from these launches provided the first evidence of radiation associated with aurora borealis.[3]

Soviet Union

The R-5 missile, 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)[4]:242 underwent its first series of eight test launches from 15 March to 23 May, 1953. After two failures, the third rocket, launched 2 April, marked the beginning of streak of success. Seven more missiles were launched between 30 October and December, all of which reached their targets. A final series of launches, designed to test modifications made in response to issues with the first series, was scheduled for mid-1954.[5]:100101

Vehicle development

U.S. Air Force

Development of the Atlas, the nation's first ICBM proceeded slowly throughout 1953. Without firm figures as to the weight and dimension of a thermonuclear device (the U.S. tested its first H-Bom in November 1952, the U.S.S.R. announced their first successful test in August 1953), it was not known if the Atlas could deliver an atomic bomb payload.

In spring 1953, Colonel Bernard Schriever, an assistant in development planning at The Pentagon and a proponent of long-ranged ballistic missiles, pushed to obtain accurate characteristics of a nuclear payload. Trevor Gardner, special assistant for research and development to the new Secretary of the Air force, Harold Talbott, responded by organizing the Strategic Missiles Evaluation Committee or "Teapot Committee" comprising eleven of the top scientists and engineers in the country. Their goal would be to determine if a nuclear payload could be made small enough to fit on the Atlas rocket. If so, the importance of the committee's members would allow such findings to accelerate Atlas development. By October, committee member John von Neumann had completed his report on weights and figures indicating that smaller, more powerful warheads within Atlas' launch capability would soon be available. Pending test verification of von Neumann's theoretical results, the Air Force began revising the Atlas design for the projected nuclear payload.[6]

U.S. Army

The first production Redstone, a surface-to-surface missile capable of delivering nuclear or conventional warheads to a range of 200 miles (320 km), was delivered on 27 July 1953. A Redstone R&D missile was flight tested on 20 August 1953.[7]

Soviet Union

In his brief tenure as Director of NII-88, responsible for the production of all Soviet ballistic missiles, engineer Mikhail Yangel chafed professionally with OKB-1 (formerly NII-88 Section 3) Chief Designer, Sergei Korolev, whom he had previously reported to as Deputy Chief Designer of the bureau. To relieve this tension, on 4 October 1953, Yangel was demoted to NII-88 Chief Engineer and assigned responsibility for production of missiles at State Union Plant No. 586 in Dnepropetrovsk. This plant under, Vasiliy Budnik, had been tasked on 13 February 1953 with developing the R-12 missile, possessing a performance similar to that of the R-5 (range of 2,000 kilometres (1,200 mi) vs. 1,200 kilometres (750 mi)) but using storable propellants so that it could be stored at firing readiness for extended periods of time.[5]:113114

At the end of 1953, at a meeting of the Presidium of the Supreme Soviet, it was determined that a transportable thermonuclear device be developed (as opposed to the one detonated in August, which was stationary). It as further determined that an ICBM be developed to carry said bomb. As no ICBMs existed at the time, in reality or even in planning, development of a nuclear capable R-5 (dubbed the "R-5M") was ordered.[4]:275

Launches

Date and time (UTC) Rocket Flight number Launch site LSP
Payload
(⚀ = CubeSat)
Operator Orbit Function Decay (UTC) Outcome
Remarks

February

10 February
21:09
Aerobee RTV-N-10 White Sands - Launch Complex 35 NRL
NRL Suborbital Mass spectrometry10 FebruarySuccessful
Apogee: 137 kilometres (85 mi)[8]
12 February
07:09
Aerobee RTV-N-10 White Sands LC-35 NRL
NRL Suborbital Mass spectrometry12 FebruarySuccessful
Apogee: 137.3 kilometres (85.3 mi)[8]
18 February
06:50
Aerobee XASR-SC-2 White Sands LC-35 US Air Force
GRENADES US Air Force Suborbital Aeronomy18 FebruarySuccessful
Apogee: 106.9 kilometres (66.4 mi)[8]
18 February
06:50
Aerobee RTV-A-1a Holloman AFB Launch Complex A ARDC
ARDC Suborbital Test18 FebruarySuccessful
Apogee: 117.5 kilometres (73.0 mi)[8]

March

1 March R-1 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test1 MarchSuccessful[9]
5 March R-1 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test5 MarchSuccessful[9]
15 March R-5 Pobeda Kapustin Yar OKB-1
OKB-1 Suborbital Missile test15 MarchLaunch failure
Maiden flight of R-5 Pobeda[10]
18 March R-5 Pobeda Kapustin Yar OKB-1
OKB-1 Suborbital Missile test18 MarchLaunch failure[10]
19 March R-1 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test19 MarchSuccessful[9]

April

2 April R-5 Pobeda Kapustin Yar OKB-1
OKB-1 Suborbital Missile test2 AprilSuccessful
First successful R-5 launch[10]
8 April R-5 Pobeda Kapustin Yar OKB-1
OKB-1 Suborbital Missile test8 AprilLaunch failure
14 April
15:47
Aerobee RTV-A-1a Holloman AFB Launch Complex A ARDC
ARDC Suborbital Test14 AprilSuccessful
Apogee: 122.3 kilometres (76.0 mi)[8]
23 April
19:33
Aerobee XASR-SC-2 White Sands - Launch Complex 35 US Air Force
SPHERE US Air Force Suborbital Aeronomy23 AprilSuccessful
Apogee: 124 kilometres (77 mi)[8]
24 April
10:19
Aerobee XASR-SC-2 White Sands LC-35 US Air Force
GRENADES US Air Force Suborbital Aeronomy24 AprilSuccessful
Apogee: 107.8 kilometres (67.0 mi)[8]
April R-5 Pobeda Kapustin Yar OKB-1
OKB-1 Suborbital Missile test Successful
Apogee: 300 kilometres (190 mi)

May

11 May R-1 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test19 MarchSuccessful[9]
20 May
14:04
Aerobee RTV-A-1a Holloman AFB Launch Complex A ARDC
Airglow-3 ARDC Suborbital Aeronomy20 MaySuccessful
Apogee: 114.3 kilometres (71.0 mi)[8]
21 May
15:47
Aerobee RTV-A-1a Holloman LC-A ARDC
Airglow-4 ARDC Suborbital Aeronomy21 MaySuccessful
Apogee: 114.3 kilometres (71.0 mi)[8]
23 May R-5 Pobeda Kapustin Yar OKB-1
OKB-1 Suborbital Missile test23 MaySuccessful
Apogee: 300 kilometres (190 mi)
May R-5 Pobeda Kapustin Yar OKB-1
OKB-1 Suborbital Missile test Successful
Apogee: 300 kilometres (190 mi)
May R-5 Pobeda Kapustin Yar OKB-1
OKB-1 Suborbital Missile test Successful
Apogee: 300 kilometres (190 mi)

June

3 June R-1 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test3 JuneSuccessful
Apogee: 150 kilometres (93 mi)
26 June
19:10
Aerobee RTV-A-1a Holloman AFB Launch Complex A ARDC
AF / Utah Ionosphere 3 Ionosphere mission ARDC Suborbital Ionospheric26 JuneSuccessful
Apogee: 135.2 kilometres (84.0 mi)[8]

July

1 July
17:52
Aerobee RTV-A-1a Holloman AFB Launch Complex A ARDC
AF / Utah Ionosphere 4 Ionosphere mission ARDC Suborbital Ionospheric1 JulySuccessful
Apogee: 138.4 kilometres (86.0 mi)[8]
6 July R-1 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test6 JulySuccessful[9]
14 July
15:30
Aerobee RTV-A-1a Holloman LC-A ARDC
ARDC Suborbital Solar UV14 JulySuccessful
Apogee: 103 kilometres (64 mi)[8]
18 July
22:27
Deacon Rockoon USS Staten Island, Atlantic Ocean Launch Site 11, Launch Point 1 US Navy
SUI-8 University of Iowa Suborbital Aeronomy/Ionospheric18 JulyLaunch failure
Apogee: 11 kilometres (6.8 mi)[11]
19 July
10:30
Deacon Rockoon USS Staten Island, Atlantic Ocean Launch Site 11, Launch Point 2 US Navy
SUI-9 University of Iowa Suborbital Aeronomy/Ionospheric19 JulyLaunch failure
Apogee: 11 kilometres (6.8 mi)[11]
19 July
15:53
Deacon Rockoon USS Staten Island, Atlantic Ocean Launch Site 11, Launch Point 3 US Navy
SUI-10 University of Iowa Suborbital Aeronomy/Ionospheric19 JulyLaunch failure
Apogee: 11 kilometres (6.8 mi)[11]
19 July
21:57
Deacon Rockoon USS Staten Island, Atlantic Ocean Launch Site 11, Launch Point 4 US Navy
SUI-11 University of Iowa Suborbital Aeronomy/Ionospheric19 JulyLaunch failure
Apogee: 11 kilometres (6.8 mi)[11]
23 July
09:47
Aerobee RTV-A-1a Holloman LC-A ARDC
ARDC Suborbital Aeronomy23 JulySuccessful
Apogee: 95.6 kilometres (59.4 mi)[8]
24 July
16:40
Deacon Rockoon USS Staten Island, Atlantic Ocean Launch Site 11, Launch Point 5 US Navy
SUI-12 University of Iowa Suborbital Aeronomy/Ionospheric24 JulyLaunch failure
Apogee: 11 kilometres (6.8 mi)[11]
29 July
09:41
Deacon Rockoon USS Staten Island, Atlantic Ocean Launch Site 11, Launch Point 6 US Navy
SUI-13 University of Iowa Suborbital Aeronomy/Ionospheric29 JulySuccessful
Apogee: 90 kilometres (56 mi)[11]

August

3 August
18:28
Deacon Rockoon USS Staten Island, Atlantic Ocean Launch Site 11, Launch Point 7 US Navy
SUI-14 University of Iowa Suborbital Aeronomy/Ionospheric3 AugustLaunch failure
Apogee: 11 kilometres (6.8 mi)[11]
5 August
21:54
Deacon Rockoon USS Staten Island, Atlantic Ocean Launch Site 11, Launch Point 21 US Navy
Naval Research Laboratory Suborbital Aeronomy5 August
Apogee: 80 kilometres (50 mi);[11] first of six 1953 flights, three of which reached altitude and returned data[3]
6 August
15:07
Deacon Rockoon USS Staten Island, Atlantic Ocean Launch Site 11, Launch Point 8 US Navy
SUI-15 University of Iowa Suborbital Aeronomy/Ionospheric6 AugustLaunch failure
Apogee: 11 kilometres (6.8 mi)[11]
6 August
18:40
Deacon Rockoon USS Staten Island, Atlantic Ocean Launch Site 11, Launch Point 9 US Navy
SUI-16 University of Iowa Suborbital Aeronomy/Ionospheric6 AugustLaunch failure
Apogee: 96 kilometres (60 mi)[11]
8 August
15:09
Deacon Rockoon USS Staten Island, Atlantic Ocean Launch Site 11, Launch Point 22 US Navy
Naval Research Laboratory Suborbital Aeronomy8 August
Apogee: 80 kilometres (50 mi);[11] second of six 1953 flights, three of which reached altitude and returned data[3]
9 August
05:54
Deacon Rockoon USS Staten Island, Atlantic Ocean Launch Site 11, Launch Point 10 US Navy
SUI-17 University of Iowa Suborbital Aeronomy/Ionospheric9 AugustSuccessful
Apogee: 100 kilometres (62 mi)[11]
9 August
19:15
Deacon Rockoon USS Staten Island, Atlantic Ocean Launch Site 11, Launch Point 23 US Navy
Naval Research Laboratory Suborbital Aeronomy9 AugustLaunch failure
Apogee: 38 kilometres (24 mi);[11] third of six 1953 flights, three of which reached altitude and returned data[3]
11 August
17:09
Deacon Rockoon USS Staten Island, Atlantic Ocean Launch Site 11, Launch Point 24 US Navy
Naval Research Laboratory Suborbital Aeronomy11 August
Apogee: 80 kilometres (50 mi);[11] fourth of six 1953 flights, three of which reached altitude and returned data[3]
30 August
14:00
Deacon Rockoon USS Eastwind, Atlantic Ocean Launch Site 11, Launch Point 11 US Navy
SUI-18 University of Iowa Suborbital Aeronomy/Ionospheric30 AugustLaunch failure
Apogee: 11 kilometres (6.8 mi)[11]
30 August
16:20
Deacon Rockoon USS Eastwind, Atlantic Ocean Launch Site 11, Launch Point 12 US Navy
SUI-19 University of Iowa Suborbital Aeronomy/Ionospheric30 AugustLaunch failure
Apogee: 11 kilometres (6.8 mi)[11]
30 August
20:46
Deacon Rockoon USS Eastwind, Atlantic Ocean Launch Site 11, Launch Point 13 US Navy
SUI-20 University of Iowa Suborbital Aeronomy/Ionospheric30 AugustSuccessful
Apogee: 100 kilometres (62 mi)[11]

September

1 September
05:05
Aerobee XASR-SC-2 White Sands - Launch Complex 35 US Air Force
GRENADES US Air Force Suborbital Aeronomy1 SeptemberSuccessful
Apogee: 107.8 kilometres (67.0 mi)[8]
3 September
09:50
Deacon Rockoon USS Eastwind, Atlantic Ocean Launch Site 11, Launch Point 14 US Navy
SUI-21 University of Iowa Suborbital Aeronomy/Ionospheric3 SeptemberSuccessful
Apogee: 90 kilometres (56 mi)[8]
3 September
11:51
Deacon Rockoon USS Eastwind, Atlantic Ocean Launch Site 11, Launch Point 15 US Navy
SUI-22 University of Iowa Suborbital Aeronomy/Ionospheric3 SeptemberSuccessful
Apogee: 100 kilometres (62 mi)[8]
3 September
14:05
Deacon Rockoon USS Eastwind, Atlantic Ocean Launch Site 11, Launch Point 16 US Navy
SUI-23 University of Iowa Suborbital Aeronomy/Ionospheric3 SeptemberSuccessful
Apogee: 100 kilometres (62 mi)[8]
4 September
03:59
Deacon Rockoon USS Eastwind, Atlantic Ocean Launch Site 11, Launch Point 25 US Navy
Naval Research Laboratory Suborbital Aeronomy/Ionospheric4 September
Apogee: 70 kilometres (43 mi);[11] fifth of six 1953 flights, three of which reached altitude and returned data[3]
4 September
15:51
Deacon Rockoon USS Eastwind, Atlantic Ocean Launch Site 11, Launch Point 26 US Navy
Naval Research Laboratory Suborbital Aeronomy/Ionospheric4 September
Apogee: 70 kilometres (43 mi);[11] sixth of six 1953 flights, three of which reached altitude and returned data[3]
5 September
05:36
Aerobee XASR-SC-1 White Sands LC-35 US Air Force
GRENADES US Air Force Suborbital Aeronomy5 SeptemberSuccessful
Apogee: 105.5 kilometres (65.6 mi)[8]
15 September
15:02
Aerobee RTV-A-1a Holloman AFB Launch Complex A ARDC
Airglow-5 ARDC Suborbital Aeronomy15 SeptemberPartial launch failure
Apogee: 32.2 kilometres (20.0 mi) (Early cut-off due to a thrust chamber burn-through; subsequent shots incorporated improved chamber cooling)[8]
29 September
20:05
Aerobee RTV-A-1a Holloman LC-A ARDC
Sphere ARDC Suborbital Aeronomy29 SeptemberSuccessful
Apogee: 58 kilometres (36 mi)[8]

October

1 October R-1 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test1 OctoberSuccessful[12]
1 October R-1 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test1 OctoberSuccessful[12]
1 October R-2 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test1 OctoberSuccessful[13]
1 October R-2 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test1 OctoberSuccessful[13]
7 October
17:00
Aerobee RTV-A-1a Holloman AFB Launch Complex A ARDC
ARDC Suborbital Solar7 OctoberSuccessful
Apogee: 99.8 kilometres (62.0 mi)[8]
10 October R-1 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test10 OctoberSuccessful
Apogee: 100 kilometres (62 mi)
10 October R-2 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test10 OctoberSuccessful[13]
16 October R-1 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test16 OctoberSuccessful[9]
17 October R-1 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test17 OctoberSuccessful[9]
19 October R-1 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test19 OctoberSuccessful[9]
20 October R-1 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test20 OctoberSuccessful[9]
24 October R-2 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test24 OctoberSuccessful[13]
26 October R-1 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test26 OctoberSuccessful[9]
27 October R-1 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test27 OctoberSuccessful[9]
28 October R-1 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test28 OctoberSuccessful[9]
28 October R-1 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test28 OctoberSuccessful[9]
30 October R-5 Pobeda Kapustin Yar OKB-1
OKB-1 Suborbital Missile test30 OctoberSuccessful
Apogee: 300 kilometres (190 mi)

November

1 November R-1 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test1 NovemberSuccessful[12]
1 November R-1 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test1 NovemberSuccessful[12]
1 November R-1 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test1 NovemberSuccessful[12]
1 November R-1 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test1 NovemberSuccessful[12]
2 November
18:32
Aerobee RTV-A-1a Holloman AFB Launch Complex A ARDC
AF / Utah Ionosphere 5 Ionosphere mission ARDC Suborbital Ionospheric2 NovemberSuccessful
Apogee: 120.7 kilometres (75.0 mi)[8]
3 November
18:15
Aerobee Holloman LC-A ARDC
AF / Utah Ionosphere 6 Ionosphere mission ARDC Suborbital Ionospheric3 NovemberSuccessful
Apogee: 121 kilometres (75 mi)[8]
12 November R-1 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test12 NovemberSuccessful[9]
15 November R-1 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test15 NovemberSuccessful[12]
15 November R-1 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test15 NovemberSuccessful[9]
Apogee: 100 kilometres (62 mi)
19 November
22:40
Aerobee RTV-N-10 White Sands - Launch Complex 35 NRL
NRL Suborbital Aeronomy/Solar19 NovemberSuccessful
Apogee: 112.6 kilometres (70.0 mi)[8]
24 November R-1 Kapustin Yar OKB-1
OKB-1 Suborbital Missile test24 NovemberSuccessful[9]
25 November
15:46
Aerobee RTV-N-10 White Sands LC-35 NRL
NRL Suborbital Aeronomy/Solar25 NovemberSuccessful
Apogee: 95.1 kilometres (59.1 mi)[8]

December

1 December
15:30
Aerobee RTV-N-10 White Sands - Launch Complex 35 NRL
NRL Suborbital Aeronomy/Solar1 DecemberSuccessful
Apogee: 129.6 kilometres (80.5 mi)[8]
9 December R-5 Pobeda Kapustin Yar OKB-1
OKB-1 Suborbital Missile test9 DecemberSuccessful
Apogee: 300 kilometres (190 mi)
December R-5 Pobeda Kapustin Yar OKB-1
OKB-1 Suborbital Missile test Successful
Apogee: 300 kilometres (190 mi)

Suborbital launch summary

By country

Soviet Union: 21USA: 20

Country Launches Successes Failures Partial
failures
Unknown Remarks
 Soviet Union4442020
 United States4641420

By rocket


Rocket Country Launches Successes Failures Partial failures Unknown Remarks
Viking (second model) United States10010
Aerobee RTV-N-10 United States55000
Aerobee XASR-SC-1 United States11000
Aerobee XASR-SC-2 United States44000
Aerobee RTV-A-1a United States1211100
UoI Deacon rockoon United States167090Maiden flight
NRL Deacon rockoon United States73310Maiden flight
R-1 Soviet Union2525000
R-2 Soviet Union414000
R-5 Soviet Union1513020

References

  1. Voosen, Paul (24 July 2018). "Outer space may have just gotten a bit closer". Science. doi:10.1126/science.aau8822. Retrieved 1 April 2019.
  2. Milton W. Rosen (1955). The Viking Rocket Story. New York: Harper & Brothers. pp. 204–221. OCLC 317524549.
  3. George Ludwig (2011). Opening Space Research. Washington D.C.: geopress. pp. 18–32. OCLC 845256256.
  4. Boris Chertok (June 2006). Rockets and People, Volume II: Creating a Rocket Industry. Washington D.C.: NASA. OCLC 946818748.
  5. Asif A. Siddiqi. Challenge to Apollo: The Soviet Union and the Space Race, 1945-1974 (PDF). Washington D.C.: NASA. OCLC 1001823253.
  6. John L. Chapman (1960). Atlas The Story of a Missile. New York: Harper & Brothers. pp. 71–73. OCLC 492591218.
  7. "Installation History 1953 - 1955". U.S. Army Aviation and Missile Life Cycle Management Command. 2017. Retrieved 1 February 2021.
  8. Wade, Mark. "Aerobee". Retrieved 2 February 2021.
  9. Wade, Mark. "R-1 8A11". Retrieved 7 January 2021.
  10. Wade, Mark. "R-5". Retrieved 2 February 2021.
  11. Wade, Mark. "Deacon Rockoon". Retrieved 8 January 2021.
  12. Wade, Mark. "R-1". Retrieved 2 February 2021.
  13. Wade, Mark. "R-2". Retrieved 7 December 2020.


This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.