Synergistic use of high and low thrust propulsion systems for piloted missions to Mars

View on Open Library

Synergistic use of high and low thrust propulsion systems for piloted missions to Mars

by James Hunter Gilland

No reviews yet

First published: 1992 1 language

Subjects

Thrust Space flight to Mars Rocket engines

Reviews

Log in or sign up to write a review.

No reviews yet. Be the first!

More by James Hunter Gilland

NEP mission sensitivities to system performance

NEP mission sensitivities to system perf...

Multimegawatt electric propulsion system design considerations

Multimegawatt electric propulsion system...

Mission and system optimization of nuclear electric propulsion vehicles for Lunar and Mars missions

Mission and system optimization of nucle...

Combined high and low thrust propulsion for fast piloted Mars missions

Combined high and low thrust propulsion ...

You Might Also Like

Sevier-age thrust fault structures control the location of base- and precious-metal mining districts in the Oquirrh Mountains, Utah

Sevier-age thrust fault structures contr...

Edwin Wilson Tooker

Thrust

Richard Noble

Optimal pitch thrust-vector angle and benefits for all flight regimes

Optimal pitch thrust-vector angle and be...

Glenn B. Gilyard

Two-dimensional converging-diverging rippled nozzles at transonic speeds

Two-dimensional converging-diverging rip...

John R. Carlson

Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring

Flight-determined subsonic longitudinal ...

Kenneth W. Iliff

Thrust-induced effects on subsonic longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration

Thrust-induced effects on subsonic longi...

P. Frank Quinto