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R-1D
Part of V-2
Russian short range ballistic suborbital launch vehicle. The R-1B version was designed for scientific research at altitudes of up to 100 km, including winds aloft, the ionosphere, and effects of spaceflight and recovery of living animals.
Status: Retired 1954. First Launch: 1954-06-26. Last Launch: 1954-07-07. Number: 3 . Gross mass: 13,400 kg (29,500 lb). Height: 14.10 m (46.20 ft). Diameter: 1.65 m (5.41 ft). Apogee: 100 km (60 mi).
Family:
short range ballistic,
suborbital launch vehicle.
Country:
Russia.
Launch Sites:
Kapustin Yar,
Kapustin Yar V-2.
Stages:
R-1 stage.
Agency:
Korolev bureau.
1954 June 26 - .
13:24 GMT - .
Launch Site:
Kapustin Yar.
Launch Complex:
Kapustin Yar V-2.
LV Family:
V-2.
Launch Vehicle:
R-1D.
- Test / biology / ionosphere / aeronomy mission - .
Nation: Russia.
Agency: Korolev bureau.
Apogee: 106 km (65 mi).
1954 July 2 - .
Launch Site:
Kapustin Yar.
Launch Complex:
Kapustin Yar V-2.
LV Family:
V-2.
Launch Vehicle:
R-1D.
- Test / biology / ionosphere / aeronomy mission - .
Nation: Russia.
Agency: Korolev bureau.
Apogee: 100 km (60 mi). Payload, instruments, left and right animal containers all recovered. Smoke container failed. Carried dogs Lyza and Ryjik..
1954 July 7 - .
Launch Site:
Kapustin Yar.
Launch Complex:
Kapustin Yar V-2.
LV Family:
V-2.
Launch Vehicle:
R-1D.
- Test / biology / ionosphere / aeronomy mission - .
Nation: Russia.
Agency: Korolev bureau.
Apogee: 100 km (60 mi). Payload recovered; left animal container, smoke container..
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