Zobrazeno 1 - 10
of 41
pro vyhledávání: '"Barry Hellman"'
Comparisons of Measured and Modeled Aero-thermal Distributions for Complex Hypersonic Configurations
Publikováno v:
55th AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4a0eebc67ba3f05e85e68d9131247eea
https://doi.org/10.2514/6.2017-0264
https://doi.org/10.2514/6.2017-0264
Publikováno v:
AIAA SPACE 2016.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::41cfa30aa0f737c563a58af95aff4843
https://doi.org/10.2514/6.2016-5320
https://doi.org/10.2514/6.2016-5320
Publikováno v:
AIAA SPACE 2015 Conference and Exposition.
This paper investigates using a fully reusable launch vehicle to deliver humanitarian supplies to a crisis region. Missions to three different reference locations were analyzed. The intention of this paper is to examine the feasibly of using this typ
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::48a87139156161f7a96b1ee5a8226e7e
https://doi.org/10.2514/6.2015-4491
https://doi.org/10.2514/6.2015-4491
Publikováno v:
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference.
Generation Orbit Launch Services, Inc. (GO) is developing GOLauncher 1, a hypersonic testbed capable of extended duration testing at high dynamic pressure, high Mach number flight conditions. These trajectories are referred to as “suppressed” tra
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ed072991b1d90361a40e3493d6e33d6d
https://doi.org/10.2514/6.2015-3688
https://doi.org/10.2514/6.2015-3688
Autor:
Barry Hellman
Publikováno v:
AIAA SPACE 2014 Conference and Exposition.
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 respon
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::03f4f52f65fc07852cbad294dad8dbb0
https://doi.org/10.2514/6.2014-4206
https://doi.org/10.2514/6.2014-4206
Publikováno v:
AIAA SPACE 2013 Conference and Exposition.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4e2802255a6cd9066051782593bf5ee2
https://doi.org/10.2514/6.2013-5531
https://doi.org/10.2514/6.2013-5531
Publikováno v:
AIAA SPACE 2013 Conference and Exposition.
Any vehicle which will be subjected to a wide range of flight conditions must have sufficient control authority to maintain vehicle attitude at all times, favoring designs which exhibit small pitching moments at each relevant flight condition. Design
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5e7f8350a1251cb0d8b5101be09cc010
https://doi.org/10.2514/6.2013-5332
https://doi.org/10.2514/6.2013-5332
Publikováno v:
AIAA SPACE 2012 Conference & Exposition.
The assumptions associated with modeling the Return to Launch Site (RTLS) trajectory for a Hybrid Launch Vehicle (HLV) are analyzed and documented in this study. The key assumptions that are identified come from the trajectory optimizer behavior. Spe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cea5752d8aec36148d2a11622d6a9de4
https://doi.org/10.2514/6.2012-5209
https://doi.org/10.2514/6.2012-5209
Publikováno v:
AIAA SPACE 2012 Conference & Exposition.
Partially reusable launch vehicle systems, featuring a reusable first stage and expendable upper stage(s), have been investigated as options for the next generation Air Force launch vehicle to meet future spacelift needs. An important area of researc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e5d1350fd307dc169d4f2d9603f43b73
https://doi.org/10.2514/6.2012-5281
https://doi.org/10.2514/6.2012-5281
Publikováno v:
AIAA SPACE 2012 Conference & Exposition.
The Air Force previously identified the reusable first stage concept as a promising approach to meet its future space lift needs. The reusable first stage consists of an autonomous, reusable, rocket-powered first stage with an expendable upper stage
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c66e1509ff6b3e13345794c74dfad09c
https://doi.org/10.2514/6.2012-5280
https://doi.org/10.2514/6.2012-5280