Mission requirements and constraints of 2-stage booster and spacecraft; both stages are manned, and employ lifting-entry configurations and current technologies to gain recoverable and reusable form; trajectory parameters including conditions of velocity, acceleration, altitude, and dynamic pressure are shown; propulsion system; aerodynamic and structural configuration, Astro performance and summary of structural design criteria and materials characteristics; recovery system; logistics and ground support, launch cost comparison and cost summary for 100 flights. (formerly Astronautics and Aerospace Eng)
Astro concept
Astronautics Aeronautics
Astronautics and Aeronautics ; 2 , n 1
1964
10 pages
Article (Journal)
English
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ASTRO-TOURISMS: A CONCEPT AND POSSIBILITY IN NEPAL
TIBKAT | 2020
|NTIS | 1991
|Online Contents | 1994
|NTRS | 1991
|Engineering Index Backfile | 1942
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