Lars Pepermans, Sebastian Oliver Scholts, Esmée Menting, Thomas Britting, Antonio López Rivera, Sowndariya Dhiyaneeswaran, Wesley L. J. R. Toussaint, Thomas C. Bosboom, Bram Koops
{"title":"Stratos IV大包络先进降落伞系统的集成","authors":"Lars Pepermans, Sebastian Oliver Scholts, Esmée Menting, Thomas Britting, Antonio López Rivera, Sowndariya Dhiyaneeswaran, Wesley L. J. R. Toussaint, Thomas C. Bosboom, Bram Koops","doi":"10.1007/s42423-022-00098-5","DOIUrl":null,"url":null,"abstract":"<div><p>The Large Envelope Advanced Parachute System (LEAPS) is developed as a means of recovering the flight data to prove that a student-built sounding rocket, Stratos IV, has reached space. Several design modifications are outlined in this work. The drogue parachute is deployed using a hot gas deployment system to save mass and volume and to increase reliability. The main parachute has been changed to a Disk-Gap-Band parachute as it is better testable in the Open Jet Facility, a subsonic wind tunnel of Delft University of Technology. A heat shield is included to protect the parachute system during atmospheric re-entry. The key benefit of this work is creating a reliable and supersonic parachute recovery system for the safe recovery of flight data located in the sounding rocket's nose cone.</p></div>","PeriodicalId":100039,"journal":{"name":"Advances in Astronautics Science and Technology","volume":"5 4","pages":"295 - 308"},"PeriodicalIF":0.0000,"publicationDate":"2022-06-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":"{\"title\":\"Integration of the Large Envelope Advanced Parachute System in Stratos IV\",\"authors\":\"Lars Pepermans, Sebastian Oliver Scholts, Esmée Menting, Thomas Britting, Antonio López Rivera, Sowndariya Dhiyaneeswaran, Wesley L. J. R. Toussaint, Thomas C. Bosboom, Bram Koops\",\"doi\":\"10.1007/s42423-022-00098-5\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><p>The Large Envelope Advanced Parachute System (LEAPS) is developed as a means of recovering the flight data to prove that a student-built sounding rocket, Stratos IV, has reached space. Several design modifications are outlined in this work. The drogue parachute is deployed using a hot gas deployment system to save mass and volume and to increase reliability. The main parachute has been changed to a Disk-Gap-Band parachute as it is better testable in the Open Jet Facility, a subsonic wind tunnel of Delft University of Technology. A heat shield is included to protect the parachute system during atmospheric re-entry. The key benefit of this work is creating a reliable and supersonic parachute recovery system for the safe recovery of flight data located in the sounding rocket's nose cone.</p></div>\",\"PeriodicalId\":100039,\"journal\":{\"name\":\"Advances in Astronautics Science and Technology\",\"volume\":\"5 4\",\"pages\":\"295 - 308\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2022-06-28\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"1\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Advances in Astronautics Science and Technology\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://link.springer.com/article/10.1007/s42423-022-00098-5\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Advances in Astronautics Science and Technology","FirstCategoryId":"1085","ListUrlMain":"https://link.springer.com/article/10.1007/s42423-022-00098-5","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Integration of the Large Envelope Advanced Parachute System in Stratos IV
The Large Envelope Advanced Parachute System (LEAPS) is developed as a means of recovering the flight data to prove that a student-built sounding rocket, Stratos IV, has reached space. Several design modifications are outlined in this work. The drogue parachute is deployed using a hot gas deployment system to save mass and volume and to increase reliability. The main parachute has been changed to a Disk-Gap-Band parachute as it is better testable in the Open Jet Facility, a subsonic wind tunnel of Delft University of Technology. A heat shield is included to protect the parachute system during atmospheric re-entry. The key benefit of this work is creating a reliable and supersonic parachute recovery system for the safe recovery of flight data located in the sounding rocket's nose cone.