Skip to content

Home/Archive/NASA NTRS

NASA NTRS · 19630010255

LAUNCH WINDOWS FOR HIGHLY ECCENTRIC ORBITS

View original source ↗Export metadata ↓

Abstract

Launch windows for highly eccentric satellite orbits

Explore related subjects

LAUNCH WINDOW SATELLITE LAUNCHING ORBIT CALCULATION ECCENTRICITY

Keep this discovery

Explore connections, maps & timelines

Shute, B. E.. 1963-01-01. LAUNCH WINDOWS FOR HIGHLY ECCENTRIC ORBITS. https://ntrs.nasa.gov/citations/19630010255

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

KEEP EXPLORING

Related reports

NASA NTRS1967

A computer simulation of the orbital launch window problem.

Digital computer simulation of orbital launch window problem for departure-trajectory analyses

LAUNCH WINDOW↗

NASA NTRS1965

A preliminary analysis of direct-ascent launch window extension using a dogleg maneuver

Data showing effect of executing dogleg maneuver on Surveyor direct-ascent launch window lengths and instantaneous impact point earth traces

LAUNCH WINDOW↗

NASA NTRS1965

Imp-c- orbit and launch time analysis

IMP-C - orbit and launch time analysis

LAUNCH WINDOW↗