¿Cuáles son el perihelio y el afelio de la segunda etapa del Falcon Heavy que contiene el Tesla después de la misión de ayer?
Parece que el tweet de Musk fue erróneo, y el afelio de la órbita estaría más cerca de 1,71 AU, en lugar de 2,61 AU. Ver el tuit de Jonathan McDowell .
Esto concuerda con la proyección de la órbita que ahora se muestra en los Horizontes de JPL :QR= 9.86...E-01 & AD= 1.711...
2458158.500000000 = A.D. 2018-Feb-09 00:00:00.0000 TDB
EC= 2.688810432654559E-01 QR= 9.860573082453878E-01 IN= 1.101912591245855E+00
OM= 3.175070416981074E+02 W = 1.772620363138233E+02 Tp= 2458153.729308890179
N = 6.292640287243981E-01 MA= 3.002024307551933E+00 TA= 5.405918374698258E+00
A = 1.348696130995557E+00 AD= 1.711334953745726E+00 PR= 5.720968998176613E+02
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
JDTDB Julian Day Number, Barycentric Dynamical Time
EC Eccentricity, e
QR Periapsis distance, q (au)
IN Inclination w.r.t XY-plane, i (degrees)
OM Longitude of Ascending Node, OMEGA, (degrees)
W Argument of Perifocus, w (degrees)
Tp Time of periapsis (Julian Day Number)
N Mean motion, n (degrees/day)
MA Mean anomaly, M (degrees)
TA True anomaly, nu (degrees)
A Semi-major axis, a (au)
AD Apoapsis distance (au)
PR Sidereal orbit period (day)
El encabezado explica que la fuente de los datos es la telemetría de la propia 3.ª etapa, que se deriva de su GPS y otros datos internos:
Revised: Feb 07, 2018 Tesla Roadster (spacecraft) -143205
Tesla Roadster (Starman, 2018-017A)
Dummy payload from first launch of SpaceX Falcon Heavy launch vehicle
consisting of a standard Tesla Roadster automobile and a spacesuit-wearing
mannequin nicknamed Starman.
Also includes a Hot Wheels toy model Roadster on the car's dash with a
mini-Starman inside. A data storage device placed inside the car contains
a copy of Isaac Asimov's "Foundation" novels. A plaque on the attachment
fitting between the Falcon Heavy upper stage and the Tesla is etched with
the names of more than 6,000 SpaceX employees.
After orbiting the Earth for 6 hours, a third-stage burn-to-depletion
was completed at approximately 02:30 UTC Feb 7, placing the dummy payload
in a heliocentric orbit having a perihelion of 0.99 au and aphelion
~1.7 au.
Payload mass: ~1250 Kg
This trajectory is a ballistic propagation derived from a post-injection
state provided by SpaceX on 2018-Feb-7, and is based on internal GPS data.
Prediction errors could increase significantly over time due to unmodeled
solar presure, thermal radiation, or outgassing accelerations that are not
characterized.
Launched: 2018-Feb-06 20:45 UTC by Falcon Heavy (FH) from Kennedy Space
Center, USA (launchpad 39A)
0,98 UA y 2,61 UA. Mira este tuit .
Pedro
usuario20636
UH oh