Skip to content

Home/Archive/NASA NTRS

NASA NTRS · 19670041888

Trajectory design for planetary mission analysis.

View original source ↗Export metadata ↓

Abstract

Trajectory design and computer programs for planetary mission analysis

Explore related subjects

COMPUTER PROGRAM PLANETARY EXPLORATION TRAJECTORY ANALYSIS

Keep this discovery

Explore connections, maps & timelines

Ross, S.. 1966-01-01. Trajectory design for planetary mission analysis.. https://ntrs.nasa.gov/citations/19670041888

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

KEEP EXPLORING

Related reports

NASA NTRS1967

A least-squares deconvolution technique for the photoelectric Fabry-Perot spectrometer.

Least squares deconvolution technique for reducing Fabry-Perot spectrometer data to Voigt profiles

COMPUTER PROGRAM↗

NASA NTRS1967

Trajectory optimization program /TOP/.

Steepest-ascent optimization program developed for flight path of current vehicles, particularly supersonic transport vehicles

COMPUTER PROGRAM↗

NASA NTRS1967

Rapid determination of near-optimum linear pitch programs for rocket boosters.

Linear segment pitch rate program for near optimum trajectory for rocket boosters

COMPUTER PROGRAM↗