Matches in SemOpenAlex for { <https://semopenalex.org/work/W1995166343> ?p ?o ?g. }
Showing items 1 to 72 of
72
with 100 items per page.
- W1995166343 endingPage "347" @default.
- W1995166343 startingPage "333" @default.
- W1995166343 abstract "The paper presents a synthesis of the performance and technical feasibility assessment of 7 reusable launcher types, comprising 13 different vehicles, studied by European Industry for ESA in the ESA Winged Launcher Study in the period January 1988 to May 1994. The vehicles comprised single-stage-to-orbit (SSTO) and two-stage-to-orbit (TSTO) vehicles, propelled by either air-breathing/rocket propulsion or entirely by rocket propulsion. The results showed that an SSTO vehicle of the HOTOL-type, propelled by subsonic combustion air-breathing/rocket engines could barely deliver the specified payload mass and was aerodynamically unstable; that a TSTO vehicle of the Saenger type, employing subsonic combustion airbreathing propulsion in its first stage and rocket propulsion in its second stage, could readily deliver the specified payload mass and was found to be technically feasible and versatile; that an SSTO vehicle of the NASP type, propelled by supersonic combustion airbreathing/rocket propulsion was able to deliver a reduced payload mass, was very complex and required very advanced technologies; that an air-launched rocket propelled vehicle of the Interim HOTOL type, although technically feasible, could deliver only a reduced payload mass, being constrained by the lifting capability of the carrier airplane; that three different, entirely rocket-propelled vehicles could deliver the specified payload mass, were technically feasible but required relatively advanced technologies." @default.
- W1995166343 created "2016-06-24" @default.
- W1995166343 creator A5005373051 @default.
- W1995166343 creator A5033655252 @default.
- W1995166343 date "1996-02-01" @default.
- W1995166343 modified "2023-10-18" @default.
- W1995166343 title "Performance and technical feasibility comparison of reusable launch systems: A synthesis of the ESA winged launcher studies" @default.
- W1995166343 cites W2990670722 @default.
- W1995166343 doi "https://doi.org/10.1016/0094-5765(96)00049-5" @default.
- W1995166343 hasPublicationYear "1996" @default.
- W1995166343 type Work @default.
- W1995166343 sameAs 1995166343 @default.
- W1995166343 citedByCount "5" @default.
- W1995166343 countsByYear W19951663432013 @default.
- W1995166343 countsByYear W19951663432016 @default.
- W1995166343 countsByYear W19951663432018 @default.
- W1995166343 crossrefType "journal-article" @default.
- W1995166343 hasAuthorship W1995166343A5005373051 @default.
- W1995166343 hasAuthorship W1995166343A5033655252 @default.
- W1995166343 hasConcept C1034443 @default.
- W1995166343 hasConcept C105923489 @default.
- W1995166343 hasConcept C116575374 @default.
- W1995166343 hasConcept C127413603 @default.
- W1995166343 hasConcept C134066672 @default.
- W1995166343 hasConcept C146978453 @default.
- W1995166343 hasConcept C158379750 @default.
- W1995166343 hasConcept C165850701 @default.
- W1995166343 hasConcept C171146098 @default.
- W1995166343 hasConcept C178790620 @default.
- W1995166343 hasConcept C178802073 @default.
- W1995166343 hasConcept C185592680 @default.
- W1995166343 hasConcept C187878255 @default.
- W1995166343 hasConcept C31258907 @default.
- W1995166343 hasConcept C41008148 @default.
- W1995166343 hasConcept C83104080 @default.
- W1995166343 hasConceptScore W1995166343C1034443 @default.
- W1995166343 hasConceptScore W1995166343C105923489 @default.
- W1995166343 hasConceptScore W1995166343C116575374 @default.
- W1995166343 hasConceptScore W1995166343C127413603 @default.
- W1995166343 hasConceptScore W1995166343C134066672 @default.
- W1995166343 hasConceptScore W1995166343C146978453 @default.
- W1995166343 hasConceptScore W1995166343C158379750 @default.
- W1995166343 hasConceptScore W1995166343C165850701 @default.
- W1995166343 hasConceptScore W1995166343C171146098 @default.
- W1995166343 hasConceptScore W1995166343C178790620 @default.
- W1995166343 hasConceptScore W1995166343C178802073 @default.
- W1995166343 hasConceptScore W1995166343C185592680 @default.
- W1995166343 hasConceptScore W1995166343C187878255 @default.
- W1995166343 hasConceptScore W1995166343C31258907 @default.
- W1995166343 hasConceptScore W1995166343C41008148 @default.
- W1995166343 hasConceptScore W1995166343C83104080 @default.
- W1995166343 hasIssue "4-8" @default.
- W1995166343 hasLocation W19951663431 @default.
- W1995166343 hasOpenAccess W1995166343 @default.
- W1995166343 hasPrimaryLocation W19951663431 @default.
- W1995166343 hasRelatedWork W1523192790 @default.
- W1995166343 hasRelatedWork W1915571629 @default.
- W1995166343 hasRelatedWork W2007373756 @default.
- W1995166343 hasRelatedWork W2316642151 @default.
- W1995166343 hasRelatedWork W2317376656 @default.
- W1995166343 hasRelatedWork W2318161451 @default.
- W1995166343 hasRelatedWork W27760488 @default.
- W1995166343 hasRelatedWork W2787786155 @default.
- W1995166343 hasRelatedWork W3200024818 @default.
- W1995166343 hasRelatedWork W4243634161 @default.
- W1995166343 hasVolume "38" @default.
- W1995166343 isParatext "false" @default.
- W1995166343 isRetracted "false" @default.
- W1995166343 magId "1995166343" @default.
- W1995166343 workType "article" @default.