FRINK Linked Data Fragments server

Matches in SemOpenAlex for { <https://semopenalex.org/work/W2313803402> ?p ?o ?g. }

• W2313803402 abstract "An investigation into new vehicle configurations appropriate for efficiently carrying small payloads to orbit with fully reusable vehicles. A baseline VTHL SSTO was modified to deliver a 2,000 Ib payload into a polar orbit. In addition, subsonic aircraft air launch assisted SSTO vehicles were considered. A POST trajectory model was modified to analyze varying air launch vehicles. POST output was used in CONS12 to perform weights and sizing calculations for the vehicles. The VTHL. SSTO showed a 43% reduction in dry weight for a payload reduction of 92%. The air launch LH2LOX vehicle weighs much less than the VTHL concept, but still has a gross weight of 1.37 million Ib. The keroseneLOX air launch vehicle produces a higher gross weight than the hydrogen vehicle. Analysis indicates that the weight of the subsonic airplane providing the launch assist will be much greater than the weight savings over the VTHL concept. * Graduate Student, Aerospace Engineering, Student Member AIM + Graduate Student, Aerospace Engincering, Member AIAA Associate Professor, Aerospace Engineering, Associate Fellow AIAA This paper is dcclared a work of thc U S Govcrnnicnt and is not subject to copyright protection in the United States. Introduction The space shuttle was designed in the 1970’s. Its concept came from research and development for the next generation of the Earth-to-orbit vehicle to replace the Apollo project vehicles and establish a reusable, low cost, and highly efficient new multi-purpose Earth-to-orbit system. At present, the space shuttle is still the most state-of-the-art and highly efficient manned Earth-to-orbit vehicle available. However, operation of the space shuttle costs much more than planned because of the requirement for high quality maintenance, the need for much manpower, and some degree of inefficiency. NASA uses the space shuttle for all manned missions no small, which leads to inefficiency. For hture space missions, vehicle size should be chosen for each mission purpose such that high efficiency can be achieved. Furthermore, to reduce the cost of missions and the risk to humans, a more efficient and safer Earth-toorbit vehicle must be used. Thus, a new transportation system has to be developed. matter whether the payload size is large or b The primary purpose of this study is to consider new vehicle configurations appropriate for individual missions and with high efficiency. Since seeking of post-spaceshuttle configurations has begun, many ideas have been introduced (Ref 1-6). For example, the U.S.A.F. concept “Black Horse” is a single stage horizontal takeoff spacecraft with aerial refueling, and “Pegasus” is a reusable 4 stage Earth-to-orbit vehicle using a reusable airplane as the first stage. Other examples are the X-34 project and NASP. Except for “Pegasus” these v" @default.
• W2313803402 created "2016-06-24" @default.
• W2313803402 creator A5025729935 @default.
• W2313803402 creator A5060229783 @default.
• W2313803402 creator A5069063005 @default.
• W2313803402 date "1995-07-10" @default.
• W2313803402 modified "2023-09-25" @default.
• W2313803402 title "Analysis of concepts for SSTO" @default.
• W2313803402 cites W2103869179 @default.
• W2313803402 doi "https://doi.org/10.2514/6.1995-2953" @default.
• W2313803402 hasPublicationYear "1995" @default.
• W2313803402 type Work @default.
• W2313803402 sameAs 2313803402 @default.
• W2313803402 citedByCount "2" @default.
• W2313803402 crossrefType "proceedings-article" @default.
• W2313803402 hasAuthorship W2313803402A5025729935 @default.
• W2313803402 hasAuthorship W2313803402A5060229783 @default.
• W2313803402 hasAuthorship W2313803402A5069063005 @default.
• W2313803402 hasConcept C106125477 @default.
• W2313803402 hasConcept C127413603 @default.
• W2313803402 hasConcept C134066672 @default.
• W2313803402 hasConcept C146978453 @default.
• W2313803402 hasConcept C158379750 @default.
• W2313803402 hasConcept C167740415 @default.
• W2313803402 hasConcept C178802073 @default.
• W2313803402 hasConcept C29829512 @default.
• W2313803402 hasConcept C31258907 @default.
• W2313803402 hasConcept C39432304 @default.
• W2313803402 hasConcept C41008148 @default.
• W2313803402 hasConceptScore W2313803402C106125477 @default.
• W2313803402 hasConceptScore W2313803402C127413603 @default.
• W2313803402 hasConceptScore W2313803402C134066672 @default.
• W2313803402 hasConceptScore W2313803402C146978453 @default.
• W2313803402 hasConceptScore W2313803402C158379750 @default.
• W2313803402 hasConceptScore W2313803402C167740415 @default.
• W2313803402 hasConceptScore W2313803402C178802073 @default.
• W2313803402 hasConceptScore W2313803402C29829512 @default.
• W2313803402 hasConceptScore W2313803402C31258907 @default.
• W2313803402 hasConceptScore W2313803402C39432304 @default.
• W2313803402 hasConceptScore W2313803402C41008148 @default.
• W2313803402 hasLocation W23138034021 @default.
• W2313803402 hasOpenAccess W2313803402 @default.
• W2313803402 hasPrimaryLocation W23138034021 @default.
• W2313803402 hasRelatedWork W1494013211 @default.
• W2313803402 hasRelatedWork W1941077008 @default.
• W2313803402 hasRelatedWork W1983228462 @default.
• W2313803402 hasRelatedWork W1985341690 @default.
• W2313803402 hasRelatedWork W1988701496 @default.
• W2313803402 hasRelatedWork W2002723657 @default.
• W2313803402 hasRelatedWork W2069212299 @default.
• W2313803402 hasRelatedWork W2079616330 @default.
• W2313803402 hasRelatedWork W2112139275 @default.
• W2313803402 hasRelatedWork W2148801922 @default.
• W2313803402 hasRelatedWork W2182804958 @default.
• W2313803402 hasRelatedWork W2315529137 @default.
• W2313803402 hasRelatedWork W2318739659 @default.
• W2313803402 hasRelatedWork W2326144398 @default.
• W2313803402 hasRelatedWork W2327482129 @default.
• W2313803402 hasRelatedWork W254214345 @default.
• W2313803402 hasRelatedWork W26906052 @default.
• W2313803402 hasRelatedWork W3165220723 @default.
• W2313803402 hasRelatedWork W1580746103 @default.
• W2313803402 hasRelatedWork W1640856561 @default.
• W2313803402 isParatext "false" @default.
• W2313803402 isRetracted "false" @default.
• W2313803402 magId "2313803402" @default.
• W2313803402 workType "article" @default.