Skip to content

Home/Archive/NASA NTRS

NASA NTRS · 19660045962

Simplified midcourse guidance techniques.

Slater, G. L.·Stern, R. G.

View original source ↗Export metadata ↓

Abstract

Six midcourse guidance techniques, noting Earth- Mars and Earth-Venus trajectory with small and large injection error

Explore related subjects

EARTH-MARS RENDEZVOUS TRAJECTORY INTERPLANETARY NAVIGATION MIDCOURSE GUIDANCE

Keep this discovery

Explore connections, maps & timelines

Slater, G. L., Stern, R. G.. 1966-01-01. Simplified midcourse guidance techniques.. https://ntrs.nasa.gov/citations/19660045962

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

KEEP EXPLORING

Related reports

NASA NTRS1967

Simulation of total equilibrium shock layer radiation for three typical entry body shapes.

Total equilibrium shock layer radiation data for Martian entry body shapes at various angles of attack extrapolated to trajectory condition

EARTH-MARS RENDEZVOUS TRAJECTORY↗

NASA NTRS1966

Manned Mars trips using Venus flyby modes.

Venus swingby used to decelerate manned spacecraft returning from Mars

EARTH-MARS RENDEZVOUS TRAJECTORY↗

NASA NTRS1965

Mariner 4 flight path to mars.

Mariner IV flight path to Mars gives same order of accuracy as Ranger, demonstrating high performance of Earth-based radio guidance coupled with single-impulse midcourse correction

EARTH-MARS RENDEZVOUS TRAJECTORY↗