Optimal staging of reusable launch vehicles considering velocity losses
This paper proposes an optimal staging method for reusable launch vehicles considering velocity losses. The proposed method expands a traditional stage optimization approach for expendable launch vehicles by introducing the descent phase of the separated stage and combining it with the trajectory op...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Jo, Byeong-Un [verfasserIn] |
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| Format: |
E-Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2021transfer abstract |
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| Schlagwörter: |
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| Übergeordnetes Werk: |
Enthalten in: Mo1474 The Role of EUS Examination and EUS-Guided Fine Needle Aspiration Biopsy for Evaluation of Gastric Subepithelial Lesions: a Large Single Center Experience - Baysal, Birol ELSEVIER, 2015, Amsterdam [u.a.] |
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| Übergeordnetes Werk: |
volume:109 ; year:2021 ; pages:0 |
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| DOI / URN: |
10.1016/j.ast.2020.106431 |
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| 520 | |a This paper proposes an optimal staging method for reusable launch vehicles considering velocity losses. The proposed method expands a traditional stage optimization approach for expendable launch vehicles by introducing the descent phase of the separated stage and combining it with the trajectory optimization procedure. For a reusable stage, the structural ratios responsible for its ascent and landing phases are defined to formulate the optimal sizing problem and optimized along with variables for traditional staging problems. An optimal staging case study on a reusable launch vehicle demonstrates the effectiveness of the proposed method. | ||
| 520 | |a This paper proposes an optimal staging method for reusable launch vehicles considering velocity losses. The proposed method expands a traditional stage optimization approach for expendable launch vehicles by introducing the descent phase of the separated stage and combining it with the trajectory optimization procedure. For a reusable stage, the structural ratios responsible for its ascent and landing phases are defined to formulate the optimal sizing problem and optimized along with variables for traditional staging problems. An optimal staging case study on a reusable launch vehicle demonstrates the effectiveness of the proposed method. | ||
| 650 | 7 | |a Soft landing |2 Elsevier | |
| 650 | 7 | |a Reusable launch vehicle |2 Elsevier | |
| 650 | 7 | |a Return to launch site |2 Elsevier | |
| 650 | 7 | |a Launch vehicle design |2 Elsevier | |
| 650 | 7 | |a Optimal sizing |2 Elsevier | |
| 650 | 7 | |a Trajectory optimization |2 Elsevier | |
| 700 | 1 | |a Ahn, Jaemyung |4 oth | |
| 773 | 0 | 8 | |i Enthalten in |n Elsevier Science |a Baysal, Birol ELSEVIER |t Mo1474 The Role of EUS Examination and EUS-Guided Fine Needle Aspiration Biopsy for Evaluation of Gastric Subepithelial Lesions: a Large Single Center Experience |d 2015 |g Amsterdam [u.a.] |w (DE-627)ELV013466232 |
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10.1016/j.ast.2020.106431 doi /cbs_pica/cbs_olc/import_discovery/elsevier/einzuspielen/GBV00000000001263.pica (DE-627)ELV052701905 (ELSEVIER)S1270-9638(20)31113-5 DE-627 ger DE-627 rakwb eng 610 VZ 600 670 VZ 51.00 bkl Jo, Byeong-Un verfasserin aut Optimal staging of reusable launch vehicles considering velocity losses 2021transfer abstract nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier This paper proposes an optimal staging method for reusable launch vehicles considering velocity losses. The proposed method expands a traditional stage optimization approach for expendable launch vehicles by introducing the descent phase of the separated stage and combining it with the trajectory optimization procedure. For a reusable stage, the structural ratios responsible for its ascent and landing phases are defined to formulate the optimal sizing problem and optimized along with variables for traditional staging problems. An optimal staging case study on a reusable launch vehicle demonstrates the effectiveness of the proposed method. This paper proposes an optimal staging method for reusable launch vehicles considering velocity losses. The proposed method expands a traditional stage optimization approach for expendable launch vehicles by introducing the descent phase of the separated stage and combining it with the trajectory optimization procedure. For a reusable stage, the structural ratios responsible for its ascent and landing phases are defined to formulate the optimal sizing problem and optimized along with variables for traditional staging problems. An optimal staging case study on a reusable launch vehicle demonstrates the effectiveness of the proposed method. Soft landing Elsevier Reusable launch vehicle Elsevier Return to launch site Elsevier Launch vehicle design Elsevier Optimal sizing Elsevier Trajectory optimization Elsevier Ahn, Jaemyung oth Enthalten in Elsevier Science Baysal, Birol ELSEVIER Mo1474 The Role of EUS Examination and EUS-Guided Fine Needle Aspiration Biopsy for Evaluation of Gastric Subepithelial Lesions: a Large Single Center Experience 2015 Amsterdam [u.a.] (DE-627)ELV013466232 volume:109 year:2021 pages:0 https://doi.org/10.1016/j.ast.2020.106431 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U GBV_ILN_40 51.00 Werkstoffkunde: Allgemeines VZ AR 109 2021 0 |
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10.1016/j.ast.2020.106431 doi /cbs_pica/cbs_olc/import_discovery/elsevier/einzuspielen/GBV00000000001263.pica (DE-627)ELV052701905 (ELSEVIER)S1270-9638(20)31113-5 DE-627 ger DE-627 rakwb eng 610 VZ 600 670 VZ 51.00 bkl Jo, Byeong-Un verfasserin aut Optimal staging of reusable launch vehicles considering velocity losses 2021transfer abstract nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier This paper proposes an optimal staging method for reusable launch vehicles considering velocity losses. The proposed method expands a traditional stage optimization approach for expendable launch vehicles by introducing the descent phase of the separated stage and combining it with the trajectory optimization procedure. For a reusable stage, the structural ratios responsible for its ascent and landing phases are defined to formulate the optimal sizing problem and optimized along with variables for traditional staging problems. An optimal staging case study on a reusable launch vehicle demonstrates the effectiveness of the proposed method. This paper proposes an optimal staging method for reusable launch vehicles considering velocity losses. The proposed method expands a traditional stage optimization approach for expendable launch vehicles by introducing the descent phase of the separated stage and combining it with the trajectory optimization procedure. For a reusable stage, the structural ratios responsible for its ascent and landing phases are defined to formulate the optimal sizing problem and optimized along with variables for traditional staging problems. An optimal staging case study on a reusable launch vehicle demonstrates the effectiveness of the proposed method. Soft landing Elsevier Reusable launch vehicle Elsevier Return to launch site Elsevier Launch vehicle design Elsevier Optimal sizing Elsevier Trajectory optimization Elsevier Ahn, Jaemyung oth Enthalten in Elsevier Science Baysal, Birol ELSEVIER Mo1474 The Role of EUS Examination and EUS-Guided Fine Needle Aspiration Biopsy for Evaluation of Gastric Subepithelial Lesions: a Large Single Center Experience 2015 Amsterdam [u.a.] (DE-627)ELV013466232 volume:109 year:2021 pages:0 https://doi.org/10.1016/j.ast.2020.106431 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U GBV_ILN_40 51.00 Werkstoffkunde: Allgemeines VZ AR 109 2021 0 |
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10.1016/j.ast.2020.106431 doi /cbs_pica/cbs_olc/import_discovery/elsevier/einzuspielen/GBV00000000001263.pica (DE-627)ELV052701905 (ELSEVIER)S1270-9638(20)31113-5 DE-627 ger DE-627 rakwb eng 610 VZ 600 670 VZ 51.00 bkl Jo, Byeong-Un verfasserin aut Optimal staging of reusable launch vehicles considering velocity losses 2021transfer abstract nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier This paper proposes an optimal staging method for reusable launch vehicles considering velocity losses. The proposed method expands a traditional stage optimization approach for expendable launch vehicles by introducing the descent phase of the separated stage and combining it with the trajectory optimization procedure. For a reusable stage, the structural ratios responsible for its ascent and landing phases are defined to formulate the optimal sizing problem and optimized along with variables for traditional staging problems. An optimal staging case study on a reusable launch vehicle demonstrates the effectiveness of the proposed method. This paper proposes an optimal staging method for reusable launch vehicles considering velocity losses. The proposed method expands a traditional stage optimization approach for expendable launch vehicles by introducing the descent phase of the separated stage and combining it with the trajectory optimization procedure. For a reusable stage, the structural ratios responsible for its ascent and landing phases are defined to formulate the optimal sizing problem and optimized along with variables for traditional staging problems. An optimal staging case study on a reusable launch vehicle demonstrates the effectiveness of the proposed method. Soft landing Elsevier Reusable launch vehicle Elsevier Return to launch site Elsevier Launch vehicle design Elsevier Optimal sizing Elsevier Trajectory optimization Elsevier Ahn, Jaemyung oth Enthalten in Elsevier Science Baysal, Birol ELSEVIER Mo1474 The Role of EUS Examination and EUS-Guided Fine Needle Aspiration Biopsy for Evaluation of Gastric Subepithelial Lesions: a Large Single Center Experience 2015 Amsterdam [u.a.] (DE-627)ELV013466232 volume:109 year:2021 pages:0 https://doi.org/10.1016/j.ast.2020.106431 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U GBV_ILN_40 51.00 Werkstoffkunde: Allgemeines VZ AR 109 2021 0 |
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10.1016/j.ast.2020.106431 doi /cbs_pica/cbs_olc/import_discovery/elsevier/einzuspielen/GBV00000000001263.pica (DE-627)ELV052701905 (ELSEVIER)S1270-9638(20)31113-5 DE-627 ger DE-627 rakwb eng 610 VZ 600 670 VZ 51.00 bkl Jo, Byeong-Un verfasserin aut Optimal staging of reusable launch vehicles considering velocity losses 2021transfer abstract nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier This paper proposes an optimal staging method for reusable launch vehicles considering velocity losses. The proposed method expands a traditional stage optimization approach for expendable launch vehicles by introducing the descent phase of the separated stage and combining it with the trajectory optimization procedure. For a reusable stage, the structural ratios responsible for its ascent and landing phases are defined to formulate the optimal sizing problem and optimized along with variables for traditional staging problems. An optimal staging case study on a reusable launch vehicle demonstrates the effectiveness of the proposed method. This paper proposes an optimal staging method for reusable launch vehicles considering velocity losses. The proposed method expands a traditional stage optimization approach for expendable launch vehicles by introducing the descent phase of the separated stage and combining it with the trajectory optimization procedure. For a reusable stage, the structural ratios responsible for its ascent and landing phases are defined to formulate the optimal sizing problem and optimized along with variables for traditional staging problems. An optimal staging case study on a reusable launch vehicle demonstrates the effectiveness of the proposed method. Soft landing Elsevier Reusable launch vehicle Elsevier Return to launch site Elsevier Launch vehicle design Elsevier Optimal sizing Elsevier Trajectory optimization Elsevier Ahn, Jaemyung oth Enthalten in Elsevier Science Baysal, Birol ELSEVIER Mo1474 The Role of EUS Examination and EUS-Guided Fine Needle Aspiration Biopsy for Evaluation of Gastric Subepithelial Lesions: a Large Single Center Experience 2015 Amsterdam [u.a.] (DE-627)ELV013466232 volume:109 year:2021 pages:0 https://doi.org/10.1016/j.ast.2020.106431 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U GBV_ILN_40 51.00 Werkstoffkunde: Allgemeines VZ AR 109 2021 0 |
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10.1016/j.ast.2020.106431 doi /cbs_pica/cbs_olc/import_discovery/elsevier/einzuspielen/GBV00000000001263.pica (DE-627)ELV052701905 (ELSEVIER)S1270-9638(20)31113-5 DE-627 ger DE-627 rakwb eng 610 VZ 600 670 VZ 51.00 bkl Jo, Byeong-Un verfasserin aut Optimal staging of reusable launch vehicles considering velocity losses 2021transfer abstract nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier This paper proposes an optimal staging method for reusable launch vehicles considering velocity losses. The proposed method expands a traditional stage optimization approach for expendable launch vehicles by introducing the descent phase of the separated stage and combining it with the trajectory optimization procedure. For a reusable stage, the structural ratios responsible for its ascent and landing phases are defined to formulate the optimal sizing problem and optimized along with variables for traditional staging problems. An optimal staging case study on a reusable launch vehicle demonstrates the effectiveness of the proposed method. This paper proposes an optimal staging method for reusable launch vehicles considering velocity losses. The proposed method expands a traditional stage optimization approach for expendable launch vehicles by introducing the descent phase of the separated stage and combining it with the trajectory optimization procedure. For a reusable stage, the structural ratios responsible for its ascent and landing phases are defined to formulate the optimal sizing problem and optimized along with variables for traditional staging problems. An optimal staging case study on a reusable launch vehicle demonstrates the effectiveness of the proposed method. Soft landing Elsevier Reusable launch vehicle Elsevier Return to launch site Elsevier Launch vehicle design Elsevier Optimal sizing Elsevier Trajectory optimization Elsevier Ahn, Jaemyung oth Enthalten in Elsevier Science Baysal, Birol ELSEVIER Mo1474 The Role of EUS Examination and EUS-Guided Fine Needle Aspiration Biopsy for Evaluation of Gastric Subepithelial Lesions: a Large Single Center Experience 2015 Amsterdam [u.a.] (DE-627)ELV013466232 volume:109 year:2021 pages:0 https://doi.org/10.1016/j.ast.2020.106431 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U GBV_ILN_40 51.00 Werkstoffkunde: Allgemeines VZ AR 109 2021 0 |
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Optimal staging of reusable launch vehicles considering velocity losses |
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This paper proposes an optimal staging method for reusable launch vehicles considering velocity losses. The proposed method expands a traditional stage optimization approach for expendable launch vehicles by introducing the descent phase of the separated stage and combining it with the trajectory optimization procedure. For a reusable stage, the structural ratios responsible for its ascent and landing phases are defined to formulate the optimal sizing problem and optimized along with variables for traditional staging problems. An optimal staging case study on a reusable launch vehicle demonstrates the effectiveness of the proposed method. |
| abstractGer |
This paper proposes an optimal staging method for reusable launch vehicles considering velocity losses. The proposed method expands a traditional stage optimization approach for expendable launch vehicles by introducing the descent phase of the separated stage and combining it with the trajectory optimization procedure. For a reusable stage, the structural ratios responsible for its ascent and landing phases are defined to formulate the optimal sizing problem and optimized along with variables for traditional staging problems. An optimal staging case study on a reusable launch vehicle demonstrates the effectiveness of the proposed method. |
| abstract_unstemmed |
This paper proposes an optimal staging method for reusable launch vehicles considering velocity losses. The proposed method expands a traditional stage optimization approach for expendable launch vehicles by introducing the descent phase of the separated stage and combining it with the trajectory optimization procedure. For a reusable stage, the structural ratios responsible for its ascent and landing phases are defined to formulate the optimal sizing problem and optimized along with variables for traditional staging problems. An optimal staging case study on a reusable launch vehicle demonstrates the effectiveness of the proposed method. |
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GBV_USEFLAG_U GBV_ELV SYSFLAG_U GBV_ILN_40 |
| title_short |
Optimal staging of reusable launch vehicles considering velocity losses |
| url |
https://doi.org/10.1016/j.ast.2020.106431 |
| remote_bool |
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| author2 |
Ahn, Jaemyung |
| author2Str |
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| doi_str |
10.1016/j.ast.2020.106431 |
| up_date |
2024-07-06T16:54:11.567Z |
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7.401696 |