A-4
Germany
Original archive entry. The text, images and links below are kept as they were written.
German production version.
Subtopics
- A-4 stage LOx/Alcohol propellant rocket stage. V-2 production version.
- A-9 stage LOx/Alcohol propellant rocket stage. Winged version.
- R-1 stage LOx/Alcohol propellant rocket stage. Payload 815 / 483 kg. Range 270 km. Maximum altitude 77 km. Time of flight 5 minutes. Max velocity at burnout 1465 m/s. Accuracy 8 km in range, 4 km laterally.
- R-2 stage LOx/Alcohol propellant rocket stage. Payload 1350 / 508 kg. Range 550 km. Maximum altitude 171 km. Time of flight 7.5 minutes. Max velocity at burnout 2175 m/s. Accuracy 8 km in range, 4 km laterally.
- R-3A stage LOx/Alcohol propellant rocket stage. Further incremental upgrade of R-2. Payload 500 kg. Range 935 km. Developed from 1949 to October 1951. Cancelled, work combined with 8K14 development.
- DF-1-1 LOx/Alcohol rocket stage. 270.00 kN (60,698 lbf) thrust. Mass 14,000 kg (30,865 lb).
Related
- Family
- short range ballistic
- People
- von Braun
- Country
- Germany
- Engines
- Model 39
- Propellants
- Lox/Alcohol
- Launch Sites
- Peenemuende P7, Heidelager, Heidekraut, Peenemuende SK, Kapustin Yar, Kapustin Yar V-2
- Stages
- A-4 stage