Welcome to Air University Central Library and Fazaia Medical College Library. (Sign in with Your email. Your user name is the same as your student ID number or Employee ID number for password, please contact Circulation Staff)

Investigation of an optimal propulation system and mission profile Design for Rocket-Scramjet integrated Hypersonic Boost-Glide-Cruise Vehical

By: Material type: TextTextPublication details: Department of Aerospace Engineering Islamabad 2023Subject(s): DDC classification:
  • 621.8 DAW-MS
Tags from this library: No tags from this library for this title. Log in to add tags.
Star ratings
    Average rating: 0.0 (0 votes)
Holdings
Item type Current library Collection Call number Status Barcode
Thesis Thesis Air University Central Library Thesis Repository (5th Floor) Aerospace Avionics Engineering 621.8 DAW-MS (Browse shelf(Opens below)) Available TH0081

There are no comments on this title.

to post a comment.
Air University Sector E-9, Islamabad Paksitan
Email: librarian@au.edu.pk  Tel : +0092 51 9262612 Ext: 631