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.
Applications
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
External links
- RD-7 on авиару.рф (in Russian)
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