On feasibility of launch vehicle designs

Applied Mathematics and Computation

Volumn 164, Issue 2, 2005, Pages 295-312

  Miele, A ^a   Wang, T ^a   Williams, P N ^a  

^a RICE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; INTERPLANETARY FLIGHT; OPTIMAL CONTROL SYSTEMS; ORBITS; STRUCTURAL ANALYSIS; TAKEOFF; TRAJECTORIES;

DOUBLE-STAGE CONFIGURATION; LOW EARTH ORBIT (LEO); MULTIPLE-SUBARC GRADIENT-RESTORATION ALGORITHM (MSGRA); SINGLE-STAGE CONFIGURATION; TRIPLE-STAGE CONFIGURATION;

SPACECRAFT;

EID: 15544379343     PISSN: 00963003     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.amc.2004.06.038     Document Type: Conference Paper

References (6)

1. A. Miele, T. Wang, P.N. Williams, On feasibility of launch vehicle designs, Aero-astronautics Report 323, Rice University, 2002
2. A. Miele, T. Wang, Multiple-subarc sequential gradient-restoration algorithm and application to launch vehicle design, Aero-astronautics Report 320, Rice University, 2002
3. A. Miele, and T. Wang Multiple-subarc gradient-restoration algorithm. Part 1: Algorithm structure Journal of Optimization Theory and Applications 116 1 2003 1 17
4. A. Miele, and T. Wang Multiple-subarc gradient-restoration algorithm. Part 2: Application to a launch vehicle design Journal of Optimization Theory and Applications 116 1 2003 19 39
5. A. Miele, and S. Mancuso Optimal ascent trajectories and feasibility of next-generation orbital spacecraft Journal of Optimization Theory and Applications 97 3 1998 519 550
6. A. Miele, and S. Mancuso On feasibility of suborbital and orbital rocket-powered spacecraft Memorie della Accademia delle Scienze di Torino 24 2000 83 109