Reusable launch vehicles

Advanced electric propulsion for RLV launched geosynchronous spacecraft

Steven Oleson.

Task 4 supporting technology: densification requirements definition and test objectives

Tibok Lak.

The X-33 extended flight test range

Dale A. Mackall, Robert Sakahara, Steven E. Kremer.

Task 4 supporting technology

P.A. Hogenson, principal investigator.

Bonding and sealing evaluations for cryogenic tanks

David E. Glass.

Effective thermal conductivity of high temperature insulations for reusable launch vehicles

Kamran Daryabeigi.

Near-optimal re-entry trajectories for reusable launch vehicles

H.-C. Chou and M.D. Ardema, and J.V. Bowles.

Analytical comparison of three stiffened panel concepts

Jill M. Maloney and K. Chauncey Wu, James C. Robinson.

Structural sizing of a 25,000-lb payload, air-breathing launch vehicle for single-state-to-orbit

Joseph M. Roche and Daniel N. Kosareoval.

Affordable In-Space Transportation phase II: an advanced concepts project : October 16-17, 1996, Technical Interchange Meeting : executive summary.

Technical Interchange Meeting (1996 Huntsville, Ala.)