Studies on expander bleed cycle engines for launchers

Martin Sippel; Armin Herbertz; Chiara Manfletti; Holger Burkhardt; Takayuki Imoto; Dietrich Haeseler; Andreas Götz

Studies on expander bleed cycle engines for launchers

Martin Sippel, Armin Herbertz, Chiara Manfletti, Holger Burkhardt, Takayuki Imoto, Dietrich Haeseler, Andreas Götz

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

6 Scopus citations

Abstract

Results of theoretical investigations on expander bleed cycle engines as well as operational experience with the LE-5B rocket motor are described. Based on results of an earlier cycle analysis, an improved engine variant of a high thrust, cryogenic bleed cycle engine is analyzed. Its performance is calculated, and a preliminary engine sizing and mass analysis is carried out. Improvement options as well as growth potential of the cycle is investigated. Special attention is paid to the critical heat-transfer in the thrust chamber region. Finally, an ascent trajectory optimization and an assessment of the complete vehicle are performed to evaluate the engine as part of a future semi reusable launch system.

Original language	English
Title of host publication	39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
State	Published - 2003
Externally published	Yes
Event	39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2003 - Huntsville, AL, United States Duration: 20 Jul 2003 → 23 Jul 2003

Publication series

Name	39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Conference

Conference	39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2003
Country/Territory	United States
City	Huntsville, AL
Period	20/07/03 → 23/07/03

Cite this

@inproceedings{cd732cbf452f459e870b765935df0f07,

title = "Studies on expander bleed cycle engines for launchers",

abstract = "Results of theoretical investigations on expander bleed cycle engines as well as operational experience with the LE-5B rocket motor are described. Based on results of an earlier cycle analysis, an improved engine variant of a high thrust, cryogenic bleed cycle engine is analyzed. Its performance is calculated, and a preliminary engine sizing and mass analysis is carried out. Improvement options as well as growth potential of the cycle is investigated. Special attention is paid to the critical heat-transfer in the thrust chamber region. Finally, an ascent trajectory optimization and an assessment of the complete vehicle are performed to evaluate the engine as part of a future semi reusable launch system.",

author = "Martin Sippel and Armin Herbertz and Chiara Manfletti and Holger Burkhardt and Takayuki Imoto and Dietrich Haeseler and Andreas G{\"o}tz",

year = "2003",

language = "English",

isbn = "9781624100987",

series = "39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit",

booktitle = "39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit",

note = "39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2003 ; Conference date: 20-07-2003 Through 23-07-2003",

}

Sippel, M, Herbertz, A, Manfletti, C, Burkhardt, H, Imoto, T, Haeseler, D & Götz, A 2003, Studies on expander bleed cycle engines for launchers. in 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2003, Huntsville, AL, United States, 20/07/03.

TY - GEN

T1 - Studies on expander bleed cycle engines for launchers

AU - Sippel, Martin

AU - Herbertz, Armin

AU - Manfletti, Chiara

AU - Burkhardt, Holger

AU - Imoto, Takayuki

AU - Haeseler, Dietrich

AU - Götz, Andreas

PY - 2003

Y1 - 2003

N2 - Results of theoretical investigations on expander bleed cycle engines as well as operational experience with the LE-5B rocket motor are described. Based on results of an earlier cycle analysis, an improved engine variant of a high thrust, cryogenic bleed cycle engine is analyzed. Its performance is calculated, and a preliminary engine sizing and mass analysis is carried out. Improvement options as well as growth potential of the cycle is investigated. Special attention is paid to the critical heat-transfer in the thrust chamber region. Finally, an ascent trajectory optimization and an assessment of the complete vehicle are performed to evaluate the engine as part of a future semi reusable launch system.

AB - Results of theoretical investigations on expander bleed cycle engines as well as operational experience with the LE-5B rocket motor are described. Based on results of an earlier cycle analysis, an improved engine variant of a high thrust, cryogenic bleed cycle engine is analyzed. Its performance is calculated, and a preliminary engine sizing and mass analysis is carried out. Improvement options as well as growth potential of the cycle is investigated. Special attention is paid to the critical heat-transfer in the thrust chamber region. Finally, an ascent trajectory optimization and an assessment of the complete vehicle are performed to evaluate the engine as part of a future semi reusable launch system.

UR - http://www.scopus.com/inward/record.url?scp=84897806447&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:84897806447

SN - 9781624100987

T3 - 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

BT - 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

T2 - 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2003

Y2 - 20 July 2003 through 23 July 2003

ER -

Studies on expander bleed cycle engines for launchers

Abstract

Publication series

Conference

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