| 摘要: |
| 对固体火箭发动机前封头绝热层在加速度环境中的炭化烧蚀特性进行了实验研究，研制了烧蚀试验发动机及相应的离心试验台，用ＮＢＲ，ＥＰＤＭ绝热层模拟实际烧蚀环境进行了不同轴向加速度条件下的烧蚀试验，得到了飞行加速度对绝热层炭化烧蚀率影响规律和经验关系式。 |
| 关键词: 固体推进剂火箭发动机 隔热材料 烧蚀试验 加速度试验 |
| DOI： |
| 分类号:V435.14 |
| 基金项目: |
|
| EFFECTS OF FLIGHT ACCELERATION ON EROSION CHARACTERISTICS OF FORWARD DOME INSULATION OF SOLID ROCKET MOTORS |
|
Tian Weiping,Yu Zhenyong,Ren Quanbing,Meng Qingfu
|
|
Shaanxi Test Inst.of Chemical Power,Xi′an,710000
|
| Abstract: |
| The charring ablation characteristics of solid rocket motors forward dome insulation in the acceleration environment were investigated by experiments.The ablation test motor and corresponding centrifugal ignition test device were researched and developed.By simulating actual ablation environment,the ablation tests of NBR and EPDM insulation were performed in different axial acceleration conditions.The influential regularities and empirical formulas were obtained |
| Key words: Solid propellant rocket engine Thermal insulating material Ablation test Acceleration test |
