Crossref DOIMemberCiteFactoropen accessissn
SJIF Impact Factor 8.659 | ISSN: 2582-3930
IJSREM Logo

International Journal of Scientific Research in Engineering and Management

(Gateway to Global Scholars - An International, Scholarly, Multi-Disciplinary, Open Access Journal)

Peer-Reviewed Journal Designed to Meet UGC's Quality Parameters

HomeCurrent IssuePast IssuesPay OnlineConferencesEditorial BoardAbout UsContact Us
IJSREM

Loading article...

Follow Us

  • Google Scholar
  • ResearchGate
  • Academia.edu
  • Mendeley
  • LinkedIn
  • Facebook
  • Instagram

Journal Policies

  • Peer Review Policy
  • Publication Ethics
  • Copyright Infringement
  • Refund & Cancellation Policy
  • Terms and Conditions
  • Privacy Policy

Journal Identifiers & Licenses

  • ISSN Verified: 2582-3930ISSN Verified: 2582-3930
  • Crossref DOI: 10.55041Crossref DOI: 10.55041
  • SJIF Ranking: 08.659SJIF Ranking: 08.659
  • Licensed under CC BY 4.0Licensed under CC BY 4.0
  • ISO Certification: 9001:2015ISO Certification: 9001:2015
  • Indexed & Cited In: Google ScholarIndexed & Cited In: Google Scholar

Contact Us

International Journal of Scientific Research in Engineering and Management (IJSREM)

#62/1, New No 7, 1st Cross, 2nd Main, Ganganagar, R T Nagar, Bangalore North, Bangalore, Karnataka, India – 560032
[email protected]+91 93911 67991
logos
logos
Working Hours

Mon – Sat: 9:00 AM – 6:00 PM

Sunday: 10:00 AM – 4:00 PM

+91 93911 67991

© 2026 IJSREM – International Journal of Scientific Research in Engineering and Management. This is an open-access journal. Articles are published under the Creative Commons Attribution (CC BY 4.0) License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

DisclaimerPrivacy PolicyTerms and Conditions
ArticlePeer ReviewedOpen AccessPlagiarism Passed
Paper ID:IJSREM27498

Advancement in Aerodynamics Design for Reusable Rocket Launch Vehicle

Stream/Area:

-

Subject:

-

Paper ID:

IJSREM27498

Volume:

7 |

12 |

Dec 2023

Pages:

Publication Frequency:

Monthly (12 issues per year)

DOI
Digital Object Identifier
Not assigned

License:International Journal of Scientific Research in Engineering and Management follows the Creative Commons Attribution 4.0 (CC BY 4.0) License, allowing free use and distribution with proper attribution.

Share this article:

Authors

SR

S. Rohan

DDM

Danny Damiaio Mantero

A

Akhilesh

JS

Jasim Shaikh

Hs

Hemanth s

Sk

Shwetha kp

Author Services & Downloads

Full Articles

Abstract

The continued evolution of reusable rocket launch vehicles is creating a paradigm shift in space exploration that requires a comprehensive re-evaluation of aerodynamic design principles. This study addresses the complex interplay between aerodynamics and the sustainable development of reusable rocket launch vehicles, and highlights the significant challenges and unprecedented opportunities associated with this transformative journey. One of the biggest challenges is dealing with the complex flow phenomena encountered during launch and reentry. The complex interactions between shock waves, boundary layers and pillars require innovative aerodynamic solutions to optimize vehicle performance and ensure structural integrity. In addition, the harsh thermal environment experienced during atmospheric re-entry poses a major obstacle, necessitating the development of robust thermal protection systems that can withstand extreme temperatures and ensure cargo safety. In addition, the pursuit of cost-effective and sustainable access to space requires the exploration of new aerodynamic technologies. Active flow control mechanisms, including advanced control surfaces and flow manipulation techniques, offer promising tools to improve vehicle maneuverability and efficiency during launch and reentry phases. At the same time, the integration of advanced materials such as lightweight composites and advanced ceramics has the potential to enhance structural flexibility while minimizing overall vehicle mass, thereby optimizing fuel consumption and operating costs. decreases. Additionally, this brief highlights opportunities to use advanced computational fluid dynamics simulations and wind tunnel testing to improve aerodynamic design parameters, simplify development programs, and accelerate the realization of next-generation rocket launch vehicles. By adopting a multidisciplinary approach that combines aerodynamics, materials science, and computational modeling, the aerospace industry opens

KEYWORDS

Cite This Article

S. Rohan, Danny Damiaio Mantero, Akhilesh, Jasim Shaikh, Hemanth s, Shwetha kp, "Advancement in Aerodynamics Design for Reusable Rocket Launch Vehicle," International Journal of Scientific Research in Engineering and Management, vol. 7, no. 12, Dec 2023.

Full Article/Conclusion

References

Editorial & Review Transparency

Publication Date

12/16/2023

Peer Review Type

Double-Blind Peer Review

Review Rounds: 2

Documents

Review Report (Confidential)
Copyright Form (Office)

Article Metrics & Impact

Article Views

0

Total views since publication

PDF Downloads

1

Total downloads since publication

Geographic Reach

5

Indexing, Archiving & Preservation

Google Scholar
Academia
ResearchGate
Crossref
SSRN
Semantic Scholar
Thomson Reuters
WorldCat
Mendeley
OpenAlex
EBSCO
Zenodo

Digital Preservation: This article is permanently archived on Zenodo and complies with all data preservation standards across major indexing platforms.

Ethics, Compliance & Transparency

Plagiarism Screening

This manuscript has been checked for plagiarism using TurnitinPlagiarismChecker software.

Conflict of Interest

The authors declare no conflict of interest related to this research work.

Funding Information

No funding information available for this research.

Similar & Recommended Articles

Similar Articles by Topic

Related research in the same subject area

Loading similar articles...