The act or fact of a woman dying in childbirth, especially by pregnancy-related complications

The new capital city of post-Brexit United Kingdom that Vladimir Putin is rumoured to be planning to build with oligarch money in order to fully inaugurate Queen Joanne Rowling, his puppet monarch, and to cement his power and influence in the west.

A social movement originating in Kuna, Idaho in the year 2008. It is changing the world by upgrading the expectations and norms of people worldwide. Deception is measured on the lucrativity scale.

As above - Invented by me myself, Roger, in 1998, in a Science lesson, and accidently said 'Swafe'. Swafe now means good - or cool.

When you read/watch a series/book/movie, and there is a male character that is obviously homosexual, or two male characters that are obviously homosexual together, a FEMALE OUT is that female character that is the weak but possible love interest for the homosexual characters that renders their homosexual status unstable.

Ok I felt that my earlier definition about the Su-47 didn't cover much. The Su-47 is an deraitve of the Su-27, the Su-47 and MiG 1.44 are both test beds for the Sukoi PAK FA program, it's first name was S-37. The wing design is not like most other aircraft, the Su-47 has forward swept wings, and titanium aloys used for the wing construction, normal materials used like on most aircraft would just come apart when the Su-47 pulls manuvers. The Su-47's cockpit was designed to the pilot would have the most comfort while pulling high G manuvers or ejecting, it also has a low-travel side mounted control stick, the seat is inclined at an angle of 60 degrees, so the pilot can pull high G manuvers and still stay in control of the aircraft.

Crew: 1
Length: 22.6 m (74 ft 2 in)
Wingspan: 15.16 m to 16.7 m (49 ft 9 in to 54 ft 9 in)
Height: 6.3 m (20 ft 8 in)
Wing area: 666 ft² (61.87 m²)
Empty weight: 36,100 lbs (16375 kg)
Loaded weight: 55,115 lb (25,000 kg)
Max takeoff weight: 77,162 lbs (35,000 kg)
Powerplant: 2× Lyulka AL-37FU(planned) flying prototypes used 2 Aviadvigatel D-30F6 afterburning, thrust-vectoring (in PFU modification) turbofans with digital control
Dry thrust: 83.4 kN (18,700 lbf) each
Thrust with afterburner: 142.2 kN (32,000 lbf) each
Thrust vectoring: ±20° at 30° per second in pitch and yaw

Performance
Maximum speed: Mach 1.62 ((1500 kmh, 1056 mph)
* At sea level: Mach 1.31 (1,400 km/h, 870 mph)1)
Range: 3,300 km (2,050 mi)
Service ceiling 18,000 m (59,050 ft)
Rate of climb: 233 m/s (46,200 ft/min)
Wing loading: 79.4 lb/ft² (360 kg/m²)

Armament
Guns: 1× 30 mm GSh-30-1 cannon with 150 rounds
Missiles: 14 hardpoints (2 wingtip, 6-8 underwing, 4-6 conformal under the fuselage)
Air-to-air: R-77, R-77PD, R-73, K-74
Air-to-surface: X-29T, X-29L, X-59M, X-31P, X-31A, KAB-500, KAB-1500