Results 11 to 20 of about 1,431,155 (187)
HYBRID ROCKET PROPULSION DEVELOPMENT AND APPLICATION. [PDF]
Satellite technology is advancing. Satellite propulsion requires several desired rocket properties. This is necessary for 1 kg of payload. Launch vehicles no longer need rocket engines. Application includes satellite movement, orbit transfer, and probe and lander propulsion. Space travel is inventive and exciting.
Akshay Gharat, Vinayak Hastak
openaire +2 more sources
Robust multi-disciplinary design and optimisation of a reusable launch vehicle [PDF]
For various technical reasons, no fully reusable launch vehicle has ever been successfully constructed or operated. Nonetheless, a range of reusable hypersonic vehicles is currently being considered as a viable alternative to the expensive but more ...
Edmondo Minisci +9 more
core +4 more sources
This paper proposed a multi-objective, multi-disciplinary design optimization and multi-attribute evaluation method for the manned lunar lander descent stage.
Yang Liu +5 more
doaj +1 more source
Artificial three-body equilibria for hybrid low-thrust propulsion [PDF]
This paper proposes a new concept of creating artificial equilibrium points in the circular restricted three body problem, where the third body uses a hybrid of solar sail and solar electric propulsion.
Baig, Shahid, McInnes, Colin R.
core +4 more sources
Experimental Investigation into Closed-Loop Control for HTPB-Based Hybrid Rocket Motors
Space exploration greatly facilitates the development of advanced propulsion systems. Extensive research has shown that hybrid rocket motors have bright prospects for use in variable-thrust propulsion systems.
Guang Tan +6 more
doaj +1 more source
Hybrid Rocket Engine Design Optimization at Politecnico di Torino: A Review
Optimization of Hybrid Rocket Engines at Politecnico di Torino began in the 1990s. A comprehensive review of the related research activities carried out in the last three decades is here presented.
Lorenzo Casalino +2 more
doaj +1 more source
Displaced geostationary orbit design using hybrid sail propulsion [PDF]
Due to an increase in number of geostationary spacecraft and limits imposed by east-west spacing requirements, the geostationary orbit is becoming congested.
Biggs, James +3 more
core +4 more sources
Non-Keplerian orbits using hybrid solar sail propulsion for Earth applications [PDF]
Half a century of space technology development has provided a wealth of new space applications. However, many still remain to be explored. Examples include increased geostationary coverage and new opportunities to enhance polar observation.
Biggs, James +3 more
core +3 more sources
This paper discusses the potential use of hydrogen peroxide as oxidizer for solid rocket propulsion. While hydrogen peroxide is a liquid in normal conditions, it may be used in solid rocket motor grains.
Wioleta Kopacz +5 more
doaj +1 more source
Development of 200 N-class throttleable hybrid rocket motor for lunar module application
In this study, ground tests of a lab-scale hybrid rocket motor were conducted to verify the feasibility of the hybrid propulsion system for lunar lander application.
Donghee Lee, Seongjoo Han, Heejang Moon
doaj +1 more source

