Bristol Thor
From Infogalactic: the planetary knowledge core
| Thor | |
|---|---|
 |
|
| Preserved Bristol Thor | |
| Type | Ramjet |
| National origin | United Kingdom |
| Manufacturer | Bristol Aero Engines |
| First run | 1950 |
| Major applications | Bristol Bloodhound |
The Bristol Thor, latterly Bristol Siddeley BS.1009 Thor, was a 16" diameter ramjet engine developed by Bristol Aero Engines (later Bristol Siddeley Engines) for the Bristol Bloodhound anti-aircraft missile.
Although Bristol Aero Engines acquired ramjet technology from the US company Marquardt, BAE put considerable effort into developing the Thor unit,[1] including the construction of a high altitude test plant (HATP), with a supersonic test cell, at their Patchway site.
The Bloodhound Mk.1 could attain a speed of Mach 2.2, while the Mk.2 was capable of just over Mach 2.7.[2]
Contents
Variants
- BT.1 Thor
- BT.2 Thor
- BT.4 Thor
- BS.1009 Thor
Specifications (BT.2 Thor)
Data from [3]
General characteristics
- Type: Ramjet
- Length: 103.9 in (2,639 mm)
- Diameter: 15.75 in (400 mm)
- Dry weight:
Components
- Compressor:
Performance
- Maximum thrust: (BT.1) - 5,275 lbf (23 kN) at M2.0 at sea level[4]
- Specific fuel consumption: 2.5 lb/lbf-hr (254.84 kg/kN-hr) at full thrust at sea level
- Power-to-weight ratio: 1.2
Notes
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