D. Manski

发表

Variable Area Ratio Nozzles and Dual Expander Performance.

D. Manski, 1990 .

ST-Transys Cycle Considered Subroutine Classification Application Programming Interface.

D. Manski, 1996 .

Optimization of Propulsion Cycles for Advanced Shuttles.

J. A. Martin, D. Manski, 1990 .

Plug Nozzle Flowfield Calculations for SSTO Applications

G. Krülle, G. Hagemann, D. Manski, 1995 .

Advanced Rocket Propulsion Systems for Reusable Ballistic Single-Stage-to-Orbit Vehicles BETA and Delta-Clipper.

D. Manski, A. Fina, 1994 .

ST 2000 A tool for system analysis of rockets and rocket engines

D. Manski, C. Kirsch, G. Frenken, 1999 .

Dual Expander Engine Flowfield Simulations

G. Krülle, G. Hagemann, D. Manski, 1995 .

A study on two-stage launcher with air-breathing propulsion

Nobuhiro Tanatsugu, D. Manski, R. E. Lo, 1986 .

Ariane 5/Mark II Burn-out Mass Capacity to GTO with Varying EPS Performance

D. Manski, 1995 .

Optimization of Dual Mode Rocket Engine Nozzles for SSTO Vehicles

Gerald Hagemann, D. Manski, M. Frey, 1998 .

Effects of engine cycle type on payload delivery of the future European launchers

D. Manski, 1985, STOC 1985.

Parametric Analysis and Optimization of the Vulcan Gas-Generator Cycle Engine for the Ariane 5 Launcher.

D. Manski, 1990 .

A novel feed system for the Space Shuttle payload propulsion platform

D. Manski, S. Rosen, 1976 .

Feasibility Study of Improved Expander Bleed Cycle and Expander Cycle Engines for SSTO Vehicle.

D. Manski, H. Nakatsuji, 1996 .

Plug Nozzle Flowfield Analysis.

G. Krülle, D. Manski, G. Hagemann, 1997 .

A critical assessment of dual-bell nozzles

Gerald Hagemann, D. Manski, M. Frey, 1997 .