Skip to content

Home/Archive/NASA NTRS

NASA NTRS · 19660008888

Optimum earth re-entry corridors

Blanton, H. E.·Muzyka, A.

View original source ↗Export metadata ↓

Abstract

Steepest ascent optimization procedure for reentry trajectory of manned aerospace vehicles

Explore related subjects

REENTRY TRAJECTORY STEEPEST ASCENT METHOD AEROSPACE VEHICLE MANNED SPACECRAFT

Keep this discovery

Explore connections, maps & timelines

Blanton, H. E., Muzyka, A.. 1966-03-01. Optimum earth re-entry corridors. https://ntrs.nasa.gov/citations/19660008888

Cite the original work for its findings. Save a collection to share your selection of sources.

KEEP EXPLORING

Related reports

NASA NTRS1965

A maximum principle re-entry study

Mathematical model of maximum principle of Pontryagin used to find point-to-point reentry trajectory of space vehicle

REENTRY TRAJECTORY↗

NASA NTRS1963

A LOOK AT THE REENTRY PROBLEM

Optimal trajectory and physical parameters for reentry from earth orbits and space

REENTRY TRAJECTORY↗

NASA NTRS1963

TRAJECTORY CONSIDERATIONS FOR THE RETURN TO EARTH PHASE OF LUNAR MISSIONS

Trajectory requirements for lunar injection and earth reentry conditions are considered in the return-to-earth phase of lunar missions

REENTRY TRAJECTORY↗