Dobrynin RD-7
| RD-7 | |
|---|---|
 | |
| Tu-22 bomber with RD-7 engines | |
| Type | |
National origin | Soviet Union |
| Manufacturer | |
| Designed by | Dobrynin OKB |
Major applications | Myasishchev M-50 |
The Dobrynin RD-7 or "VD-7" is a Soviet axial-flow turbojet engine.
Contents
1 Applications
2 Specifications (VD-7M)
2.1 General characteristics
2.2 Components
2.3 Performance
3 See also
4 External links
Applications
- Tupolev Tu-22
- Myasishchev M-50
- Myasishchev VM-T
- Caspian Sea Monster
Specifications (VD-7M)
General characteristics
Type: Turbojet
Length: 7300 mm
Diameter: 1410 mm
Dry weight: 3750 kg
Components
Compressor: Axial flow, 9-stage LP, 7-stage HP
Turbine: 2-stage
Performance
Maximum thrust: Dry: 10500 kgf, 16000 kgf with afterburner
Overall pressure ratio: 11
Turbine inlet temperature: 630°C
Power-to-weight ratio: 4.27
See also
Related lists
- List of aircraft engines
External links
RD-7 on авиару.рф (in Russian)
