Author: Charles L. Zola
Publisher:
ISBN:
Category : Space flight to Venus
Languages : en
Pages : 112
Book Description
Three-dimensional Trajectory Analysis for Round-trip Missions to Venus
Author: Charles L. Zola
Publisher:
ISBN:
Category : Space flight to Venus
Languages : en
Pages : 112
Book Description
Publisher:
ISBN:
Category : Space flight to Venus
Languages : en
Pages : 112
Book Description
Three-dimensional Trajectory Analysis for Round-trip Missions to Mars
Author: Gerald Knip
Publisher:
ISBN:
Category : Artificial satellites
Languages : en
Pages : 168
Book Description
Publisher:
ISBN:
Category : Artificial satellites
Languages : en
Pages : 168
Book Description
NASA Technical Note
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 1004
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 1004
Book Description
Round-trip Trajectories with Stopovers at Both Mars and Venus
Author: Edward A. Willis
Publisher:
ISBN:
Category : Interplanetary voyages
Languages : en
Pages : 34
Book Description
Publisher:
ISBN:
Category : Interplanetary voyages
Languages : en
Pages : 34
Book Description
Analysis of Trajectory Parameters for Probe and Round-trip Missions to Venus
Author: James F. Dugan
Publisher:
ISBN:
Category : Planets
Languages : en
Pages : 54
Book Description
For one-way transfers between Earth and Venus, charts are obtained that show velocity, time, and angle parameters as functions of the eccentricity and semilatus rectum of the Sun-focused vehicle conic. From these curves, others are obtained that are useful in planning one-way and round-trip missions to Venus. The analysis is characterized by circular coplanar planetary orbits, successive two-body approximations, impulsive velocity changes, and circular parking orbits at 1.1 planet radii. For round trips the mission time considered ranges from 65 to 788 days, while wait time spent in the parking orbit at Venus ranges from 0 to 467 days. Individual velocity increments, one-way travel times, and departure dates are presented for round trips requiring the minimum total velocity increment. For both single-pass and orbiting Venusian probes, the time span available for launch becomes appreciable with only a small increase in velocity-increment capability above the minimum requirement. Velocity-increment increases are much more effective in reducing travel time for single-pass probes than they are for orbiting probes. Round trips composed of a direct route along an ellipse tangent to Earth's orbit and an aphelion route result in the minimum total velocity increment for wait times less than 100 days and mission times ranging from 145 to 612 days. Minimum-total-velocity-increment trips may be taken along perihelion-perihelion routes for wait times ranging from 300 to 467 days. These wait times occur during missions lasting from 640 to 759 days.
Publisher:
ISBN:
Category : Planets
Languages : en
Pages : 54
Book Description
For one-way transfers between Earth and Venus, charts are obtained that show velocity, time, and angle parameters as functions of the eccentricity and semilatus rectum of the Sun-focused vehicle conic. From these curves, others are obtained that are useful in planning one-way and round-trip missions to Venus. The analysis is characterized by circular coplanar planetary orbits, successive two-body approximations, impulsive velocity changes, and circular parking orbits at 1.1 planet radii. For round trips the mission time considered ranges from 65 to 788 days, while wait time spent in the parking orbit at Venus ranges from 0 to 467 days. Individual velocity increments, one-way travel times, and departure dates are presented for round trips requiring the minimum total velocity increment. For both single-pass and orbiting Venusian probes, the time span available for launch becomes appreciable with only a small increase in velocity-increment capability above the minimum requirement. Velocity-increment increases are much more effective in reducing travel time for single-pass probes than they are for orbiting probes. Round trips composed of a direct route along an ellipse tangent to Earth's orbit and an aphelion route result in the minimum total velocity increment for wait times less than 100 days and mission times ranging from 145 to 612 days. Minimum-total-velocity-increment trips may be taken along perihelion-perihelion routes for wait times ranging from 300 to 467 days. These wait times occur during missions lasting from 640 to 759 days.
Technical Publications Announcements with Indexes
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1556
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1556
Book Description
Planetary Atmospheres
Author:
Publisher:
ISBN:
Category : Planets
Languages : en
Pages : 452
Book Description
Publisher:
ISBN:
Category : Planets
Languages : en
Pages : 452
Book Description
U.S. Government Research Reports
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1170
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1170
Book Description
Parametric Performance Analysis for Interplanetery Missions Utilizing First-generation Nuclear Stages
Author: Walter H. Stafford
Publisher:
ISBN:
Category : Space flight to Mars
Languages : en
Pages : 220
Book Description
Publisher:
ISBN:
Category : Space flight to Mars
Languages : en
Pages : 220
Book Description
Technical Report - Jet Propulsion Laboratory, California Institute of Technology
Author: Jet Propulsion Laboratory (U.S.)
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 598
Book Description
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 598
Book Description