Difference between revisions of "SR-91 Aurora"
Jump to navigation
Jump to search
Lafayette1 (talk | contribs) |
Lafayette1 (talk | contribs) |
||
| Line 60: | Line 60: | ||
|max takeoff weight alt=71,215 kg | |max takeoff weight alt=71,215 kg | ||
|engine (jet)= | |engine (jet)= | ||
| − | |type of jet=afterburning | + | |type of jet=Pratt & Whitney J58-1 afterburning turbojets, 32,500 lbf (145 kN) each |
|number of jets='''(Low Speed)''' 4 | |number of jets='''(Low Speed)''' 4 | ||
|thrust main=267 kN est. thrust | |thrust main=267 kN est. thrust | ||
Revision as of 19:26, 9 March 2009
| SR-91 "Aurora" | |
|---|---|
 | |
| Role | Strategic Reconnaissance Aircraft |
| Manufacturer | Rubin Design Aerospace |
| First flight | 2007 |
| Status | Testing |
| Primary users | U.S. Air Force International Space Agency |
| Produced | 2007 to present |
| Number built | 7 |
| Unit cost | Unknown |
| Developed from | SR-71 Blackbird North American X-15 XB-70 Valkyrie |
Contents
History
Design and operational details
Air inlets
Fuselage
Stealth
Fuel
Life support
Sensors and payloads
Operational history
Variants
Specifications
General characteristics
- Crew: 2 (1 pilot, 1 reconnaissance systems officer)
- Length: 35 m (115 ft)
- Wingspan: 20 m (65 ft)
- Height: 6 m (19 ft)
- Wing area: 300 m² (3,200 ft²)
- Empty weight: 29,480 kg (65,000 lb)
- Max takeoff weight: 71,215 kg (157,000 lb)
- Max takeoff weight: 157,000 lb (71,215 kg)
- Powerplant: (Low Speed) 4× Pratt & Whitney J58-1 afterburning turbojets, 32,500 lbf (145 kN) each, 267 kN est. thrust ((High Speed) 4× scramjets or pulse detonation engines) each
Performance
- Maximum speed: unknown at sea level (Mach 10 at altitude)
- Range: 9,320 mi (15,000 km)
- Service ceiling: 40,000 m (131,000 ft)
- Thrust/weight: 0.70 est.
Fuel types
- JP-7 or JP-8
- Methane, MCH, LH2 or hydrogen fuel cells.
- Possible use of liquid oxygen and hydrogen oxides.
- Possible use of MHD (MagnetoHydroDynamics) technology.
Other equipment
- Cameras
- IR sensors
- Other advanced recon sensors
