{"doi":"10.2514/6.2009-7238","title":"TBCC Propulsion for a Mach 6 Hypersonic Airplane","abstract":null,"journal":"16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference","year":2009,"id":597282,"datarank":0.5050943744979712,"base_score":3.367295829986474,"endowment":3.367295829986474,"self_citation_contribution":0.5050943744979712,"citation_network_contribution":0.0,"self_endowment_contribution":0.5050943744979712,"citer_contribution":0.0,"corpus_percentile":null,"corpus_rank":null,"citation_count":28,"citer_count":0,"citers_with_citation_signal":0,"citers_with_endowment":0,"datacite_reuse_total":0,"is_dataset":false,"is_dataset_confidence":null,"is_data_producer":false,"deposit_databanks":null,"is_oa":false,"file_count":0,"downloads":0,"has_version_chain":false,"published_date":null,"fair_score":null,"fair_percentile":null,"algorithm_id":"datarank_citation_only_1hop_v6","ranking_scope":"data_only","authors":[{"id":239862,"name":"Ming Tang","orcid":"0000-0002-6786-3201","position":1,"is_corresponding":false},{"id":1530156,"name":"Caesar Mamplata","orcid":null,"position":2,"is_corresponding":false},{"id":1530155,"name":"Steven Walker","orcid":null,"position":0,"is_corresponding":false}],"reference_count":0,"raw_metadata":{"has_enrichment":true,"resolved":true,"title":"TBCC Propulsion for a Mach 6 Hypersonic Airplane","abstract":"Hypersonic speed can be achieved through rocket-boost, air-breathing propulsion, or a high-energy state from orbit. This paper will focus on air-breathing hydrocarbon fueled hypersonic flight at Mach 6. Flight demonstration of a Mach 6 hypersonic airplane in a realistic environment will enable the future development of re-usable high-speed operational systems for strike, ISR, or other national need missions. Technologies enabling this capability are turbine-based combined cycle (TBCC) propulsion, efficient aerodynamics, high temperature structures, and thermal management techniques. The TBCC propulsion system enables complete transition from low-speed to high-speed flight and enables re-usable aircraft-like operations take-off from a conventional runway under turbojet power, acceleration to Mach 6 under combined propulsion, deceleration, and turbojet powered landing – without the need for carrier aircraft or rocket assist. The Defense Advanced Projects Agency (DARPA) Falcon Combined-Cycle Engine Technology (FaCET) and Mode Transition (MoTr) programs will ground test TBCC propulsion, a critical step to enabling flight demonstration of a Mach 6 hypersonic airplane. Mach 6 Airplane Enablers After 50 years of many stops and starts in air-breathing hypersonic research programs, there have been only two successful flight demonstrations, ASALM and X-43, as shown in Figure 1. In each case, carrier aircraft and/or rockets were required. Aerospace Plane National Aerospace Plane (NASP) National Aerospace Initiative (NAI) ASALM Ramjet HRE X-24C NHRF HST SED ARRMD X-43A Hyper-X Scramjet","is_dataset_classified":null,"base_score":3.367295829986474,"endowment":3.367295829986474,"datacite_reuse_total":0,"file_count":0,"downloads":0,"views":0,"has_version_chain":false,"is_dataset":false,"is_oa":false,"pmid":"21097893","pmcid":null,"openalex_id":"https://openalex.org/W2335549580","authors":[],"funders":[],"total_grants":0,"fwci":null,"citation_percentile":null,"influential_citations":0,"citation_trend":[{"year":2015,"count":1},{"year":2017,"count":3},{"year":2018,"count":3},{"year":2019,"count":5},{"year":2020,"count":2},{"year":2021,"count":1},{"year":2022,"count":4},{"year":2023,"count":2},{"year":2025,"count":2},{"year":2026,"count":2}],"oa_status":"closed","license":null,"oa_locations":[{"url":"http://arc.aiaa.org/doi/pdf/10.2514/6.2009-7238","host_type":"publisher"},{"url":"https://doi.org/10.2514/6.2009-7238","host_type":"conference"}],"fields_of_study":["Computational Fluid Dynamics and Aerodynamics","Gas Dynamics and Kinetic Theory","Rocket and propulsion systems research"],"mesh_terms":[],"keywords":["Aerospace engineering","Mach number","Aeronautics","Hypersonic speed","Airplane","Propulsion","Hypersonic flight","Computer science","Engineering"],"sdg_mappings":[{"sdg_number":0,"sdg_label":"Affordable and clean energy"}],"linked_datasets":[],"clinical_trials":[],"software_tools":[],"database_accessions":[],"source":"live","citation_network_status":"fetched"},"created_at":"2026-07-28T12:50:05.831209Z","pmid":null,"pmcid":null,"fwci":null,"citation_percentile":null,"influential_citations":0,"oa_status":null,"license":null,"views":0,"total_file_size_bytes":0,"version_count":0,"fair_f":null,"fair_a":null,"fair_i":null,"fair_r":null,"fair_zscore":null,"fair_rationale":null,"fair_model":null,"fair_agent_version":null,"fair_fulltext_source":null,"fair_has_llm":null,"fair_computed_at":null,"clinical_trials":[],"software_tools":[],"db_accessions":[],"linked_datasets":[],"topics":[]}