V-2 sounding rocket
V-2 Sounding Rocket | |
---|---|
Type | Single-stage |
Service history | |
In service | 1946-1952 |
Used by | United States |
Specifications | |
Mass | 13,000 kg (29,000 lb) |
Length | 14 m (45 ft 11 in) |
Diameter | 1.65 m (5 ft 5 in) |
Wingspan | 3.56 m (11 ft 8 in) |
Propellant |
|
German V-2 rockets captured by the United States Army at the end of World War II were used as sounding rockets to carry scientific instruments into the Earth's upper atmosphere, and into sub-orbital space, at White Sands Missile Range (WSMR) for a program of atmospheric and solar investigation through the late 1940s. Rocket trajectory was intended to carry the rocket about 100 miles (160 km) high and 30 miles (48 km) horizontally from WSMR Launch Complex 33. Impact velocity of returning rockets was reduced by inducing structural failure of the rocket airframe upon atmospheric re-entry. More durable recordings and instruments might be recovered from the rockets after ground impact, but telemetry was developed to transmit and record instrument readings during flight.[1]: 112–116
History
The first of 300 railroad cars of V-2 rocket components began to arrive at Las Cruces, New Mexico in July 1945 for transfer to WSMR.[2]: 246 So much equipment was taken from Germany that the Deutsches Museum later had to obtain a V-2 for an exhibit from the US.[3] In November General Electric (GE) employees began to identify, sort, and reassemble V-2 rocket components in WSMR Building 1538, designated as WSMR Assembly Building 1. The Army completed a blockhouse in WSMR Launch Area 1 in September 1945. WSMR Launch Complex 33 for the captured V-2s was built around this blockhouse.[4]
Initial V-2 assembly efforts produced 25 rockets available for launch. The Army assembled an
See also: Launches of captured V-2 rockets in the United States after 1945
Modifications
The 2,200 pounds (1,000 kg) explosive warhead in the 17 cubic feet (0.48 m3) nose cone was replaced by a package of instrumentation averaging 1,200 pounds (540 kg). Instrumentation was sometimes added to the control compartment, in the rear motor section, between the fuel tanks, or on the fins or skin of the rocket. Nose cone instrumentation was typically assembled at participating laboratories and flown to WSMR to be joined to the rocket in Assembly Building 1.[1]: 113-115&135
Rockets returning to Earth intact created an impact crater about 80 feet (24 m) wide and of similar depth which filled with debris to a depth of about 35 feet (11 m). In an effort to preserve instruments, dynamite was strategically placed within the airframe to be detonated at an elevation of 50 kilometres (31 mi) during downward flight at end of the high-altitude scientific observation interval. These explosives weakened the rocket structure so it would be torn apart by aerodynamic forces as it re-entered the denser lower atmosphere. Terminal velocity of tumbling fragments was reduced by an order of magnitude.[1]: 115-116&138
Performance
V-2 sounding rockets were 47 feet (14 m) long and 5 feet 5 inches (1.65 m) in diameter and weighed 28,000 pounds (13,000 kg) with a full load of liquid fuel contributing two-thirds of that weight. The fuel was consumed in the first minute of flight producing a thrust of 56,000 pounds-force (250 kN). Maximum acceleration of 6 Gs was reached at minimum fuel weight just before burnout, and vibrational accelerations were of similar magnitude during powered flight. Velocity at burnout was approximately 5,000 feet (1,500 m) per second. The rocket would typically have a small, unpredictable angular momentum at burnout causing unpredictable roll with pitch or yaw as it coasted upward approximately 75 miles (121 km). A typical flight provided an observation window of 5 minutes at altitudes above 35 miles (56 km).[1]: 135–137
Instrumentation
Servomechanisms were devised to compensate for rocket aspect changes as it tumbled after burnout. These allowed Sun-tracking devices to measure the solar electromagnetic spectrum. Limited success was achieved with parachute recovery of instrumentation, but some of the more durable instruments or recordings within the rocket airframe could withstand impact with the earth at subsonic velocities.[1]: 116&137
NRL developed a telemetry system using a 23-channel pulse-time modulation. Voltage presented to the input terminals of a given channel determined spacing between two adjacent pulses, not entirely unlike the technique of pulse-position modulation. Space between first and second pulses was determined by channel 1, between second and third pulses by channel 2, and so forth. The system made 200 samplings per second of 24 pulses. Information was transmitted via high-power frequency modulation. Ground receiving stations translated pulse spacings back into voltages which were applied to a bank of string galvanometers to make an approximately continuous record of each channel on a moving roll of film. Accuracy was within approximately 5 percent.[1]: 116&138
Scientific operations
A 1946
The first night flight of a V-2 sounding rocket began at 10:00 pm (MST) 17 December 1946 on an Applied Physics Laboratory flight. This rocket carried several explosive charges that generated artificial meteors, which could be observed photographically. The experiment package was installed by James Van Allen. Though the flight itself was photographed by observers as far away (285 mi (459 km)) as Tucson, Arizona, the charges and expected meteors were not, and it is likely they did not fire.[8]
Animals tests
The first animals sent into space were
Numerous monkeys of several species were flown by the U.S. in the 1950s and 1960s. Monkeys were implanted with sensors to measure vital signs, and many were under anesthesia during launch. The death rate among monkeys at this stage was very high: about two-thirds of all monkeys launched in the 1940s and 1950s died on missions or soon after landing.[13]
See also
- Hermes (missile program)
- RTV-G-4 Bumper
- V-2 No. 13
- Spaceflight before 1951
References
- ^ a b c d e f g h Kuiper, Gerard (1952) [1949]. The Atmospheres of the Earth and Planets. Chicago: The University of Chicago Press. pp. 112–117 & 134–138.
- ^ Ley, Willy (1958) [1944]. Rockets, Missiles and Space Travel. New York: The Viking Press. pp. 246, 253.
- ^ Ley, Willy (June 1964). "Anyone Else for Space?". For Your Information. Galaxy Science Fiction. pp. 110–128.
- ^ a b "A Brief History of White Sands Proving Ground 1941–1965" (PDF). New Mexico State University. Archived from the original (PDF) on 28 October 2014. Retrieved 19 August 2010.
- ^ a b Wade, Mark. "V-2". Archived from the original on August 20, 2016. Retrieved 7 December 2020.
- doi:10.1086/106028.
- ^ "Richard Tousey (1908 - 1997) | American Astronomical Society". aas.org. Archived from the original on 2019-08-19. Retrieved 2017-07-24.
- S2CID 122476458.
- ^ Beischer, DE; Fregly, AR (1962). "Animals and man in space. A chronology and annotated bibliography through the year 1960" (PDF). US Naval School of Aviation Medicine. ONR TR ACR-64 (AD0272581). Archived from the original on 24 March 2016. Retrieved 14 June 2011.
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: CS1 maint: unfit URL (link) - ^ UPPER AIR ROCKET SUMMARY V-2 NO. 20. postwarv2.com
- ^ "The Beginnings of Research in Space Biology at the Air Force Missile Development Center, 1946–1952". History of Research in Space Biology and Biodynamics. NASA. Archived from the original on 25 January 2008. Retrieved 31 January 2008.
- ^ "V-2 Firing Tables". White Sands Missile Range. Archived from the original on 25 January 2008. Retrieved 31 January 2008.
- ^ Gray, Tara. "A Brief History of Animals in Space". National Aeronautics and Space Administration. NASA. Retrieved 9 December 2019.