OPTIMUM TWO-PULSE PASSAGE BETWEEN ORBITS WITH SMALL INCLINATIONS AND ECCENTRICITIES,

Abstract

An analytical formulation is given of the trajectory of an optimum two-pulse flight between orbits with small inclinations and eccentricities. (Author)

Document Details

Document Type
Technical Report
Publication Date
May 15, 1965
Accession Number
AD0616282

Entities

People

  • V. S. Novoselov

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Eccentricity
  • Trajectories

Fields of Study

  • Physics

Technology Areas

  • Space
  • Space - Orbital Debris