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

Fina, A. and Manski, D. (1994) Advanced Rocket Propulsion Systems for Reusable Ballistic Single-Stage-to-Orbit Vehicles BETA and Delta-Clipper. In: 30th AIAA/ASME/SAE/ASEE Joint Conference, June 27-29, 1994; Indianapolis, IN, USA.

Full text not available from this repository.

Abstract

A single-stage-to-orbit VTOVL mission was evaluated using four different types of mixed-mode propulsion systems such as dual engines, dual mixture ratio, dual position nozzle and dual throat. VTOVL laucheners using staged combustion and gas-generator cycle engines. The single stage launcher BETA-II was taken as reference vehicle. Hydrogen and/or hydrocarbons as fuels with oxygen were used as propellants. A constant payload mass transported into low earth orbit was assumed, and the minimal effective net mass of the launcher was determined. Optimizations and variations were made for the effective net mass of the BETA-vehicle versus mixture ratios and chamber pressures.

Item URL in elib:https://elib.dlr.de/24824/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1994, pages=7,
Title:Advanced Rocket Propulsion Systems for Reusable Ballistic Single-Stage-to-Orbit Vehicles BETA and Delta-Clipper.
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Fina, A.UNSPECIFIEDUNSPECIFIED
Manski, D.UNSPECIFIEDUNSPECIFIED
Date:1994
Journal or Publication Title:30th AIAA/ASME/SAE/ASEE Joint Conference, June 27-29, 1994; Indianapolis, IN, USA
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Series Name:AIAA 94-3316
Status:Published
Keywords:Traegerraketen, Raketentriebwerke, Triebwerkszyklen, Dual-Mode Triebwerke
HGF - Research field:UNSPECIFIED
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:UNSPECIFIED
DLR - Program:W RP - Raumtransport
DLR - Research theme (Project):UNSPECIFIED
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Institut für Chemische Antriebe und Verfahrenstechnik
Deposited By: DLR-Beauftragter, elib
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 05:35

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