Hypersonic retro propulsion for reusable launch vehicles tested in the H2K wind tunnel
- Location
-
Deutsche Nationalbibliothek Frankfurt am Main
- ISSN
-
1868-2510
- Extent
-
Online-Ressource
- Language
-
Englisch
- Notes
-
online resource.
- Bibliographic citation
-
Hypersonic retro propulsion for reusable launch vehicles tested in the H2K wind tunnel ; volume:14 ; number:3 ; day:29 ; month:6 ; year:2022 ; pages:473-499 ; date:7.2022
CEAS space journal / Confederation of European Aerospace Societies ; 14, Heft 3 (29.6.2022), 473-499, 7.2022
- Creator
- Contributor
-
SpringerLink (Online service)
- DOI
-
10.1007/s12567-022-00457-w
- URN
-
urn:nbn:de:101:1-2022101322402418874049
- Rights
-
Open Access; Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
-
15.08.2025, 7:36 AM CEST
Data provider
This object is provided by:
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Associated
- Marwege, Ansgar
- Kirchheck, Daniel
- Klevanski, Josef
- Gülhan, Ali
- SpringerLink (Online service)
Other Objects (12)
Mission design for point-to-point passenger transport with reusable launch vehicles
Aerothermal databases and load predictions for Retro Propulsion-Assisted Launch Vehicles (RETALT)
Ranking of parameters influencing the cost-effectiveness of reusable heavy lift launch vehicles
Stability analysis and flight control design of the winged reusable launch vehicle ReFEx
Analysis of liquid spring damper for vertical landing reusable launch vehicle with network-based methodology
High-enthalpy hypersonic flows
Tested & Approved
Tested & Approved
Tested & Approved
Tested & approved
Tested & Approved
Tested & approved
Mission design for point-to-point passenger transport with reusable launch vehicles
Aerothermal databases and load predictions for Retro Propulsion-Assisted Launch Vehicles (RETALT)
Ranking of parameters influencing the cost-effectiveness of reusable heavy lift launch vehicles
Stability analysis and flight control design of the winged reusable launch vehicle ReFEx
Analysis of liquid spring damper for vertical landing reusable launch vehicle with network-based methodology
High-enthalpy hypersonic flows
Tested & Approved
Tested & Approved
Tested & Approved
Tested & approved
Tested & Approved
Tested & approved
Mission design for point-to-point passenger transport with reusable launch vehicles
Aerothermal databases and load predictions for Retro Propulsion-Assisted Launch Vehicles (RETALT)
Ranking of parameters influencing the cost-effectiveness of reusable heavy lift launch vehicles
Stability analysis and flight control design of the winged reusable launch vehicle ReFEx
Analysis of liquid spring damper for vertical landing reusable launch vehicle with network-based methodology
High-enthalpy hypersonic flows
Tested & Approved
Tested & Approved
Tested & Approved
Tested & approved
Tested & Approved