Synthesis of the optimum descent trajectories of a spacecraft in the atmosphere of Mars using a parachute-rocket system for a soft landing

Details Synthesis of the optimum descent trajectories of a spacecraft in the atmosphere of Mars using a parachute-rocket system for a soft landing Synthesis of the optimum descent trajectories of a spacecraft in the atmosphere of Mars using a parachute-rocket system for a soft landing

Nov 1977

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1977cosre..15..296i&link_type=associated

(Kosmicheskie Issledovaniia, vol. 15, May-June 1977, p. 346-351.) Cosmic Research, vol. 15, no. 3, Nov. 1977, p. 296-301. Transl

Physics

Descent Trajectories, Mars Landing, Parachute Descent, Soft Landing, Trajectory Optimization, Aerodynamic Brakes, Mars Atmosphere, Rockets, Weight Reduction

Scientific paper

Not Available

Affiliated with

Also associated with

No associations

Rating

Synthesis of the optimum descent trajectories of a spacecraft in the atmosphere of Mars using a parachute-rocket system for a soft landing 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 Synthesis of the optimum descent trajectories of a spacecraft in the atmosphere of Mars using a parachute-rocket system for a soft landing, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Synthesis of the optimum descent trajectories of a spacecraft in the atmosphere of Mars using a parachute-rocket system for a soft landing will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFWR-SCP-O-1131034