共 31 条
- [1] Natali M, Kenny J M, Torre L., Science and technology of polymeric ablative materials for thermal protection systems and propulsion devices: a review, Progress in Materials Science, 84, pp. 192-275, (2016)
- [2] Xie W H, Han G K, Meng S H, Et al., Development status and trend of thermal protection structure for return capsules and space probes, Acta Aeronautica et Astronautica Sinica, 40, 8, pp. 6-22, (2019)
- [3] Jiang G Q, Liu L Y., Heat Transfer of Hypersonic Gas and Ablation Thermal Protection, pp. 52-93, (2003)
- [4] Xue H F, Yao X R, Cheng H M, Et al., Current situation development of lightweight ablation materials for thermal protection, Journal of Harbin University of Science and Technology, 22, 1, pp. 123-128, (2017)
- [5] Ou D B, Chen L Z, Chen H Q, Et al., Ablation properties of silicon based composites, Aerospace Materials & Technology, 39, 1, pp. 85-87, (2009)
- [6] Sun B, Lin X S, Liu X Y, Et al., Study on ablation model of silica-reinforced composites, Journal of Astronautics, 24, 3, pp. 282-286, (2003)
- [7] Shi S B, Liang J, Fang G D., Effect of thermal physical properties on ablation properties of high silica/phenolic composite, Journal of Solid Rocket Technology, 34, 3, pp. 354-359, (2011)
- [8] Johnston C O, Gnoffo P A, Sutton K., Influence of ablation on radiative heating for earth entry, Journal of Spacecraft and Rockets, 46, 3, pp. 481-491, (2009)
- [9] Yu J J, Jiang G Q, Li Z P., Ablation and heat conduction mechanism and test validation of high viscosity SiO<sub>2</sub> materials, Acta Aerodynamica Sinica, 26, 4, pp. 462-465, (2008)
- [10] Yi F J, Liang J, Meng S H, Et al., Study on ablation mechanism and models of heatshield composites, Journal of Solid Rocket Technology, 23, 4, pp. 48-56, (2000)