Qualitative Experimental Verification of the Change of Burning Rate of Rocket Powders with Radiation Path Length

Penner S. S.

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Qualitative Experimental Verification of the Change of Burning Rate of Rocket Powders with Radiation Path Length

机译：火箭粉燃烧速率随辐射路径长度变化的定性实验验证

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Experimental studies on step‐machined powder grains indicate a small increase in the average burning rate of solid fuel rocket propellants with an increase in the radiation path length. This result is in agreement with theoretical predictions.

机译：对步进加工粉末颗粒进行的实验研究表明，固体燃料火箭推进剂的平均燃烧速率随辐射路径长度的增加而略有增加。该结果与理论预测相符。

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《Journal of Applied Physics》 |1948年第6期|共3页
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Penner S. S.;
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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);美国《生物学医学文摘》(MEDLINE);
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正文语种 eng
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专利

1. Note on ``Qualitative Experimental Verification of the Change of Burning Rate of Rocket Powders with Radiation Path Length'' [J] . Muraour Henri Journal of Applied Physics . 1949,第8期

机译：关于``具有辐射路径长度的火箭粉末燃烧速率变化的定性实验验证''的注释
2. Improvement in the burning rate of a rocket propellant through radiation curing [J] . V.G.Dedgaonkar, P.B.navle, P.G.Shrotr Radiation Physics and Chemistry . 1997,第1期

机译：通过辐射固化提高火箭推进剂的燃烧速率
3. Experimental investigation of the factors affecting the burning rate of solid rocket propellants [J] . Hayri Yaman, Veli Celik, Ercan Degirmenci Fuel . 2014,第jana期

机译：影响固体火箭推进剂燃烧速度的因素的实验研究
4. Verification of the Throttling Characteristics of Axial-Injection End-Burning type Hybrid Rockets [C] . Yuji Saito, Toshiki Yokoi, Hiroyuki Yasukochi, International astronautical congress . 2016

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5. Calculation and Experimental Verification of Longitudinal Spatial Hole Burning in High- Power Semiconductor Lasers [D] . Hao, Ting 2014

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6. Investigation of an implantable dosimeter for single-point water equivalent path length verification in proton therapy [O] . Hsiao-Ming Lu, Greg Mann, Ethan Cascio -1

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7. Verification Firings of End-Burning Type Hybrid Rockets [O] . Nagata, Harunori, Teraki, Hayato, Saito, Yuji, 2017

机译：末端燃烧式混合火箭的验证射击
8. The effect of mixing, radiation, and finite rate combustion upon the flow field and surroundings of the exhaust plumes of rocket engines burning RP1 /kerosene/ and liquid oxygen [R] . Edelman, R., Fortune, O. 1967

机译：混合，辐射和有限速率燃烧对燃烧Rp1 /煤油/液氧的火箭发动机排气羽流的流场和周围环境的影响

Qualitative Experimental Verification of the Change of Burning Rate of Rocket Powders with Radiation Path Length

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