Producing ablative thermal protection systems by additive manufacturing

References

• Glass D. Ceramic Matrix Composite (CMC) Thermal Protection Systems (TPS) and hot structures for hypersonic vehicles. AIAA. 2008; doi: 10.2514/6.2008-2682.
   Google Scholar
• Venkatapathy E. Ablators - From apollo to future missions to moon, mars and beyond. Inter Astron Congr. 2019.
   Google Scholar
• Chapline G, Rodriguez A, Snapp C, et al. NASA Engineering Innovations, 182–199.
   Google Scholar
• Malhan RK, Shembekar AV, Kabir AM, et al. Automated planning for robotic layup of composite prepreg. Rob Comput Integr Manuf. 2021;67:102020. doi: 10.1016/j.rcim.2020.102020.
   Web of Science ®Google Scholar
• Bhatt P, Malhan R, Shembekar A, et al. Expanding capabilities of additive manufacturing through use of robotics technologies: a survey. Addit Manuf. 2019;31:100933. doi: 10.1016/j.addma.2019.100933.
   Web of Science ®Google Scholar
• Graves RA, Witte WG. Flight-test analysis of Apollo heat-shield material using the pacemaker vehicle system (tech. rep.); 1968.
   Google Scholar
• White T, Hwang H, Ellerby D, et al. thermal protection system materials for sample return missions. Bull AAS. 2021;53(4) doi: 10.3847/25c2cfeb.72d83582.
   Google Scholar
• Ellerby D, Stackpoole M, Gasch M, et al. Sustaining phenolic impregnated carbon ablator (PICA) for future NASA missions including discovery and new frontiers background-PICA (tech. rep.); 2019.
   Google Scholar
• Phenolic-Impregnated Carbon Ablator (PICA) Heat Shield Technology is Used by SpaceX - NASA; 2015.
   Google Scholar
• Venkatapathy E, Ellerby D, Gage P, et al. Entry system technology readiness for ice-giant probe missions. Space Sci Rev. 2020;216(2):22. doi: 10.1007/s11214-020-0638-2.
   Web of Science ®Google Scholar
• Abdullah F, Okuyama K-I, Morimitsu A, et al. Effects of thermal cycle and ultraviolet radiation on 3D printed carbon fiber/polyether ether ketone ablator. Aerospace. 2020;7(7):95. doi: 10.3390/aerospace7070095.
   Web of Science ®Google Scholar
• Kafi A, Wu H, Langston J, et al. Evaluation of additively manufactured ultraperformance polymers to use as thermal protection systems for spacecraft. J Appl Polymer Sci. 2020;137(37) doi: 10.1002/app.49117.
   Web of Science ®Google Scholar
• Roberts T. CSIS Missile Defense Project; 2022.
   Google Scholar
• Weinzierl M. Space, the Final Economic Frontier. J Econ Perspect. 2018;32(2):173–192. doi: 10.1257/jep.32.2.173.
   Web of Science ®Google Scholar
• Hwang H, et al. Bull. AAS. 2021;53. doi: 10.3847/25C2CFEB.72D83582.
   Google Scholar
• Sun L. Thermal rheological analysis of cure process of epoxy prepreg [PhD thesis]. Baton Rouge: Louisiana State University; 2002.
   Google Scholar
• Pulci G, Tirillò J, Marra F, et al. Carbon–phenolic ablative materials for re-entry space vehicles: manufacturing and properties. Composites Part A Appl Sci Manufact. 2010;41(10):1483–1490. doi: 10.1016/j.compositesa.2010.06.010.
   Web of Science ®Google Scholar
• Cho D, Il Yoon B. Microstructural interpretation of the effect of various matrices on the ablation properties of carbon-fiber-reinforced composites. Compos Sci Technol. 2001;61(2):271–280. doi: 10.1016/S0266-3538(00)00212-8.
   Web of Science ®Google Scholar
• Kim HJ, Brunovska Z, Ishida H. Synthesis and thermal characterization of polybenzoxazines based on acetylene-functional monomers. Polymer. 1999;40(23):6565–6573. doi: 10.1016/S0032-3861(99)00046-4.
   Web of Science ®Google Scholar
• Mishra J, Rao C, Bose PSC, et al. Experimental Studies of Resin Systems for Ablative Thermal Protection System. Def Sc J. 2021;71(2):289–295. doi: 10.14429/dsj.71.16252.
   Web of Science ®Google Scholar
• Lee Y-K, Kim D-J, Kim H-J, et al. Activation energy and curing behavior of resol- and novolac-type phenolic resins by differential scanning calorimetry and thermogravimetric analysis. J of Applied Polymer Sci. 2003;89(10):2589–2596. doi: 10.1002/app.12340.
   Web of Science ®Google Scholar
• Hong F, Hodges S, Myant C, et al. Conference on Human Factors in Computing Systems-Proceedings; 2022. doi: 10.1145/3491101.3519782.
   Google Scholar