Entry of a spacecraft into an artificial-satellite orbit around a planet using aerodynamic braking in the atmosphere

Details Entry of a spacecraft into an artificial-satellite orbit around a planet using aerodynamic braking in the atmosphere Entry of a spacecraft into an artificial-satellite orbit around a planet using aerodynamic braking in the atmosphere

Jul 1975

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1975kosis..13..448i&link_type=abstract

Kosmicheskie Issledovaniia, vol. 13, July-Aug. 1975, p. 448-456. In Russian.

Physics

1

Aerodynamic Drag, Atmospheric Entry, Braking, Planetary Orbits, Spacecraft Maneuvers, Spacecraft Orbits, Acceleration (Physics), Differential Equations, Hyperbolic Trajectories, Orbit Calculation

Scientific paper

The problem is considered of placing a spacecraft with a hyperbolic trajectory into orbit around a planet by means of aerodynamic braking in the atmosphere and the subsequent application of an accelerating impulse for raising the pericenter of the orbit. The structure of the optimum equation of spacecraft motion is determined, and the rocket-dynamic maneuver is analyzed. Numerical results are given for placing a spacecraft into orbit around Mars.

Affiliated with

Also associated with

No associations

Rating

Entry of a spacecraft into an artificial-satellite orbit around a planet using aerodynamic braking in the atmosphere does not yet have a rating. At this time, there are no reviews or comments for this scientific paper.

If you have personal experience with Entry of a spacecraft into an artificial-satellite orbit around a planet using aerodynamic braking in the atmosphere, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Entry of a spacecraft into an artificial-satellite orbit around a planet using aerodynamic braking in the atmosphere will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFWR-SCP-O-1756672