Determination of the width of a corridor of re-entry into the atmosphere for the problem of launching a spacecraft into a circumplanetary orbit after braking in the atmosphere

Author： Yaroshevskii V.  

Publisher： MAIK Nauka/Interperiodica

ISSN： 0010-9525

Source： Cosmic Research, Vol.44, Iss.3, 2006-05, pp. : 236-244

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

Previous Menu Next

Abstract

Related content

Hermes Spaceplane in MBB Wind Tunnel: Aerodynamics Engineers Determine Optimum Configuration for Safe Gliding After Re-Entry into Atmosphere

By  

Aircraft Engineering, Vol. 60, Iss. 3, 1993-12 ,pp. : 10-10

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Transition of Planar Rotational Motion of an Asymmetric Spacecraft into Oscillatory Motion at Its Reentry into the Atmosphere

By Kenshov E. A.   Timbai I. A.  

Cosmic Research, Vol. 42, Iss. 3, 2004-05 ,pp. : 283-288

MAIK Nauka/Interperiodica

Access to resources Recommend Favorite

Robust algorithm of control for a maneuver in the Martian atmosphere to insert a spacecraft into the planet’s satellite orbit

By Sikharulidze Yu.   Korchagin A.   Zhukov B.  

Cosmic Research, Vol. 45, Iss. 4, 2007-08 ,pp. : 317-330

MAIK Nauka/Interperiodica

Access to resources Recommend Favorite

Features of rotational motion of a spacecraft descending in the Martian atmosphere

By Aslanov V.   Ledkov A.  

Cosmic Research, Vol. 45, Iss. 4, 2007-08 ,pp. : 331-338

MAIK Nauka/Interperiodica

Access to resources Recommend Favorite

Integrated solution to the problem of estimation and identification of a state vector of the gimballess navigation system of a reentry spacecraft

By Pogorelov V.  

Cosmic Research, Vol. 44, Iss. 3, 2006-05 ,pp. : 268-275

MAIK Nauka/Interperiodica

Access to resources Recommend Favorite