Trajectory Approaches for Launching Hypersonic Flight Tests

Autor:	Barry Hellman
Rok vydání:	2014
Předmět:	Hypersonic speed Engineering business.product_category business.industry Hypersonic flight ComputerApplications_COMPUTERSINOTHERSYSTEMS symbols.namesake Mach number Rocket Trajectory symbols Stage (hydrology) Aerospace engineering business Simulation
Zdroj:	AIAA SPACE 2014 Conference and Exposition.
DOI:	10.2514/6.2014-4206
Popis:	This paper presents some approaches towards designing trajectories for hypersonic testing at up to Mach 10 speed using a reusable rocket powered first stage. The motivation behind the paper is the DARPA XS-1 program that is focused on low cost responsive access to space of which the first stage can also be used for hypersonic testing. Trajectories were analyzed using NASA’s POST code to look at different ways of flying to Mach 10 with a reusable first stage rocket. These trajectories are good starting points for how to setup a trajectory simulation to meet hypersonic testing needs.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::03f4f52f65fc07852cbad294dad8dbb0 https://doi.org/10.2514/6.2014-4206 Zobrazit plný text záznamu