Dobrynin RD-7
| RD-7 | |
|---|---|
| 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
This article is issued from Wikipedia - version of the 10/19/2015. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.