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In a well tuned aircraft the desired and achieved roll and pitch should match to within a couple of degrees for any portion of the flight where stabilisation is enabled.</description> <expression>NAV_CONTROLLER_OUTPUT.nav_roll NAV_CONTROLLER_OUTPUT.nav_pitch degrees(ATTITUDE.roll) degrees(...
First Launch: 1991-01-08. Last Launch: 1993-12-08. Number: 2 . Gross mass: 1,434 kg (3,161 lb). NATO Missile Firing Installation - Alternate name for NAMFI. Natsionalnie Kosmichne Agentstvo Ukrayni - Alternate name for NKAU. Naugle, John E - American physicist, at NASA 1959-1981...
Apogee: 699 km (434 mi). Perigee: 694 km (431 mi). Inclination: 29.00 deg. Period: 98.70 min. Ultraviolet space telescope. Much delayed launch (from January 19, May 19, July 16, 21 and 30, August 14 and October 17, 2002; January 27, March 25 and 30, April 15 and 26 2003)....
1971-08-12 - Cosmos 434 - T2K s/n 3 - Final LK moon lander test using T2K version. Maneuver Summary: 188 km x 267 km orbit to 190 km X 1261 km orbit, delta V 266 m/s; 188 km x 1262 km orbit to 180 km X 11,384 km orbit, delta V 1333 m/s. ...
Thrust increased more than 30% from Vulcain 1. First flight 2002. Status: In development. Number: 9 . Thrust: 1,350.00 kN (303,490 lbf). Unfuelled mass: 1,800 kg (3,900 lb). Specific impulse: 434 s. Specific impulse sea level: 318 s. Height: 3.60 m (11.80 ft). Diameter: ...
Apogee: 36,105 km (22,434 mi). Perigee: 35,852 km (22,277 mi). Inclination: 0.68 deg. Period: 1,445.94 min. DSP-1 Block 14 ballistic missile launch detection satellite. Last flight of the IUS upper stage. Launch delayed from November 4, 2003, and January 17, 2003. Planned IMEX...
Apogee: 699 km (434 mi). Perigee: 694 km (431 mi). Inclination: 29.00 deg. Period: 98.70 min. Ultraviolet space telescope. Much delayed launch (from January 19, May 19, July 16, 21 and 30, August 14 and October 17, 2002; January 27, March 25 and 30, April 15 and 26 2003)....