Design feasibility via ascent optimality for next-generation spacecraft-Reference-Cited by-同舟云学术

Design feasibility via ascent optimality for next-generation spacecraft

Published:1999-12 Issue:12 Volume:45 Page:705-715
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Miele A.,Mancuso S.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference27 articles.

1. Miele, A. and Mancuso, S., Optimal ascent trajectories for a single-stage suborbital spacecraft, Aero-Astronautics Report 275, Rice University, 1997

2. Miele, A. and Mancuso, S., Optimal ascent trajectories for SSTO and TSTO spacecraft, Aero-Astronautics Report 276, Rice University, 1997

3. Miele, A. and Mancuso, S., Optimal ascent trajectories for TSTO spacecraft: extensions, Aero-Astronautics Report 277, Rice University, 1997

4. Miele, A. and Mancuso, S., Optimal ascent trajectories for SSSO, SSTO and TSTO spacecraft: extensions, Aero-Astronautics Report 278, Rice University, 1997

5. Anonymous, N. N., Access to space study, summary report, Office of Space Systems Development, NASA Headquarters, 1994

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