Trajectory design for a reusable launch vehicle demonstrator during Re-entry phase

AIAA Atmospheric Flight Mechanics Conference and Exhibit

Volumn , Issue , 2003, Pages

  Arora, Rajesh Kumar ^a   Ananthasayanam, M R ^a,b  

^a INDIAN SPACE RESEARCH ORGANISATION   (India)

^b INDIAN INSTITUTE OF SCIENCE   (India)

Author keywords

[No Author keywords available]

Indexed keywords

ASCENT PHASE; DYNAMIC PRESSURES; LANDING SITE; LIFT OFFS; PROPELLANT CONSUMPTION; REUSABLE LAUNCH VEHICLES; TRAJECTORY DESIGNS;

DESIGN; HEAT FLUX; REENTRY; REUSABILITY; ROCKETS;

TRAJECTORIES;

EID: 84896832740     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. K Singa Rao et al., "RLV Technology Demonstrator - System Definition and Preliminary Specification", VSSC Internal Report, March 2002
2. Rajesh Kumar Arora, "Reentry Trajectory Optimization: Evolutionary Approach", AIAA 2002-5466, Atlanta, Georgia, September 2002
3. Lu Xuefu, Nan Ying, "The optimal return trajectory design of space vehicle", AAS 93-348
4. David E Goldberg, "Genetic algorithm in search, optimization and machine learning", Addison - Wessley