LANZAMIENTO DIRECTO, Atlas 5 • AFSPC 5
19-may-2015 20:33
#1
![]() 4º lanzamiento de un X-37B May 20 Atlas 5 • AFSPC 5 Launch period: LANZADO Launch site: SLC-41, Cape Canaveral Air Force Station, Florida VER ONLINE: http://original.livestream.com/spaceflightnow http://www.ulalaunch.com/webcast.aspx ![]() ![]() ![]() ![]() ![]() ![]() ![]() ![]() ![]() ![]() --------------------------------------------------------- VUELOS ESPACIALES, LANZAMIENTOS EN DIRECTO, mandando cohetes a la órbita y mas allá --------------------------------------------------------- |
Editado: 20-may-2015 17:27 -
20-may-2015 13:11
#18
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Entre otras cargas menores, esta incluida LightSail-A, una vela solar. Más información: http://sail.planetary.org/ https://vine.co/v/eZtpWW0WnZY ![]()
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Editado: 20-may-2015 13:33 -
20-may-2015 13:20
#20
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Configuración del lanzador 501, 62,2m de alto, diámetro de 3,81m y 337 toneladas. Atlas V 501 Specifications Type Atlas V 501 Height 62.2m Diameter 3.81m Launch Mass 337,300kg Stage 1 Atlas Common Core Booster Boosters None Stage 2 Centaur Mass to LEO 8,123kg Mass to GTO 3,775kg First Stage Type Common Core Booster Inert Mass 21,054kg Diameter 3.81m Length 32.46m Propellant Rocket Propellant-1 (Kerosene) Oxidizer Liquid Oxygen Fuel&Oxidizer Mass 284,089kg Guidance From Centaur Propulsion RD-180 Engine (2 Chambers) Type Staged Combustion Thrust at Sea Level 3,827kN Isp SL 311s Thrust (Vacuum) 4,152kN (933,369 lbf) Isp Vac 338s Engine Length 3.56m Engine Diameter 3.15m Engine Dry Weight 5,480kg Chamber Pressure 266.8bar Nozzle Ratio 36.87 Thrust to Weight 78.22 Area Ratio 36.4 Ox. To Fuel Ratio 2.72 Attitude Control Gimbaled Engine (8 Degrees) Throttle Capability 50-100% Burn Time 253 sec Tank Pressurization Helium Avionics Flight Control, Flight Termination Telemetry, Rate Gyros, Power Stage Separation 8 Retro Rockets Interstage Adapter Type Cylindrical Interstage Adapter Diameter 3.83m Length 0.32m Mass 285kg Structure Aluminum Machined Rolled-Ring Forging C-ISA Adapter Diameter 3.83m Length 3.81m Components Interstage Adapter Aft Stub Adapter Boattail Mass 2,212kg Structure Composite Sandwich Aluminum Core Graphite Epoxy Face Sheets Centaur Upper Stage Type Centaur Diameter 3.05m Length 12.68m Inert Mass 2,243kg Propellant Liquid Hydrogen Oxidizer Liquid Oxygen Fuel&Oxidizer Mass 20,830kg Guidance Inertial Propulsion 1 RL 10A-4-2 (until 2014) Thrust 99.2kN Isp Vac 451s Engine Length 2.29m Engine Diameter 1.53m Engine Dry Weight 167kg Chamber Pressure 39bar Thrust to Weight 61 Area Ratio 84 Mixture Ratio 5.5:1 Propulsion 1 RL-10C-1 (Starting in 2014) Thrust 106.3kN Isp Vac 448.5s Engine Length 2.22m Engine Diameter 1.44m Engine Dry Weight 190kg Chamber Pressure 24bar Thrust to Weight 57 Area Ratio 130 Mixture Ratio 5.88:1 Burn Time Variable Engine Start Restartable Attitude control 4 27-N Thrusters 8 40-N Thrusters Propellant Hydrazine Payload Fairing Fairing Bisector, Sandwich Construction Epoxy Face Sheets Aluminum Honeycomb Core Boattail Fixed, Composite Sandwich Separation Linear Piston & Cylinder activated by Pyro Cord, Expanding Tube shearing a notched Frame for Horizontal Separation Type Short PLF Diameter 5.4m Length 20.7m Mass 3,524kg Type Medium PLF Diameter 5.4m Length 23.4m Mass 4,003kg Type Long PLF Diameter 5.4m Length 26.5m Mass 4,379kg |
20-may-2015 13:35
#21
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Frecuencia y modo de la vela solar para recibir las imágenes(o trozos de ellas) 437.435 NFM 9600 bps FSK. http://amsat-uk.org/2015/05/20/lightsail-1-launch/ |
20-may-2015 16:12
#23
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pillo sitio mientras arrancan, sabes cual es este bicho y que tal es? http://i.imgur.com/IX76mGA.jpg |
20-may-2015 16:44
#24
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pillo sitio
mientras arrancan, sabes cual es este bicho y que tal es? http://i.imgur.com/IX76mGA.jpg Un 11 pulgadas es ya un abertura muy seria. |
20-may-2015 16:48
#27
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.. At the request of our customer, we'll conclude live mission coverage approx 5 mins after liftoff.
Due to the top-secret nature of the payload the live launch broadcast will end about five minutes after lift off
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20-may-2015 16:53
#29
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Primer intento de lanzamiento de 17:05 a 17:15. Segundo intento de la lanzamiento de 18:42 a 18:52 |


















