Analysis of liquid spring damper for vertical landing reusable launch vehicle with network-based methodology
- Standort
-
Deutsche Nationalbibliothek Frankfurt am Main
- ISSN
-
1573-269X
- Umfang
-
Online-Ressource
- Sprache
-
Englisch
- Anmerkungen
-
online resource.
- Erschienen in
-
Analysis of liquid spring damper for vertical landing reusable launch vehicle with network-based methodology ; day:8 ; month:10 ; year:2022 ; pages:1-26
Nonlinear dynamics ; (8.10.2022), 1-26
- Urheber
-
Yue, Shuai
Titurus, Branislav
Li, Zhiqian
Wu, Chunbo
Du, Zhonghua
- Beteiligte Personen und Organisationen
-
SpringerLink (Online service)
- DOI
-
10.1007/s11071-022-07944-z
- URN
-
urn:nbn:de:101:1-2022122621104048097463
- Rechteinformation
-
Open Access; Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Letzte Aktualisierung
-
15.08.2025, 07:30 MESZ
Datenpartner
Dieses Objekt wird bereitgestellt von:
Deutsche Nationalbibliothek. Bei Fragen zum Objekt wenden Sie sich bitte an den Datenpartner.
Deutsche Nationalbibliothek. Bei Fragen zum Objekt wenden Sie sich bitte an den Datenpartner.
Beteiligte
- Yue, Shuai
- Titurus, Branislav
- Li, Zhiqian
- Wu, Chunbo
- Du, Zhonghua
- SpringerLink (Online service)
Ähnliche Objekte (12)
Investigation of the landing dynamics of a reusable launch vehicle and derivation of dimension loading for the landing leg
Comparative analysis of European vertical landing reusable first stage concepts
Design of the landing guidance for the retro-propulsive vertical landing of a reusable rocket stage
A damper
Mission design for point-to-point passenger transport with reusable launch vehicles
Ranking of parameters influencing the cost-effectiveness of reusable heavy lift launch vehicles
Hypersonic retro propulsion for reusable launch vehicles tested in the H2K wind tunnel
Stability analysis and flight control design of the winged reusable launch vehicle ReFEx
Electrical launch catapult and landing decelerator for fixed-wing airborne wind energy systems
Damper Paradies - Trottellume 0517
Hafen mit Damper, Kotor
Autonomous Automatic Takeoff and Landing of Rigid Wind Airborne Wind Energy Systems: Control Launch and Landing, 14:50-15:10, Wednesday, 16 October 2019
Investigation of the landing dynamics of a reusable launch vehicle and derivation of dimension loading for the landing leg
Comparative analysis of European vertical landing reusable first stage concepts
Design of the landing guidance for the retro-propulsive vertical landing of a reusable rocket stage
A damper
Mission design for point-to-point passenger transport with reusable launch vehicles
Ranking of parameters influencing the cost-effectiveness of reusable heavy lift launch vehicles
Hypersonic retro propulsion for reusable launch vehicles tested in the H2K wind tunnel
Stability analysis and flight control design of the winged reusable launch vehicle ReFEx
Electrical launch catapult and landing decelerator for fixed-wing airborne wind energy systems
Damper Paradies - Trottellume 0517
Hafen mit Damper, Kotor
Autonomous Automatic Takeoff and Landing of Rigid Wind Airborne Wind Energy Systems: Control Launch and Landing, 14:50-15:10, Wednesday, 16 October 2019
Investigation of the landing dynamics of a reusable launch vehicle and derivation of dimension loading for the landing leg
Comparative analysis of European vertical landing reusable first stage concepts
Design of the landing guidance for the retro-propulsive vertical landing of a reusable rocket stage
A damper
Mission design for point-to-point passenger transport with reusable launch vehicles
Ranking of parameters influencing the cost-effectiveness of reusable heavy lift launch vehicles
Hypersonic retro propulsion for reusable launch vehicles tested in the H2K wind tunnel
Stability analysis and flight control design of the winged reusable launch vehicle ReFEx
Electrical launch catapult and landing decelerator for fixed-wing airborne wind energy systems
Damper Paradies - Trottellume 0517
Hafen mit Damper, Kotor