Index of /~cantwell/AA283_Course_Material/AA283_Resources

[ICO]NameLast modifiedSizeDescription
[PARENTDIR]Parent Directory  -  
[ ]Tsiolkovsky, Exploration of the Universe with Reaction Machines 1898.pdf2019-12-16 14:02 4.2M 
[ ]Solar_Sails.pdf2017-03-20 11:17 13M 
[ ]STANJAN_write-up_by_Bill_Reynolds.pdf2010-08-09 10:56 3.4M 
[DIR]STANJAN_PC/2004-02-26 11:36 -  
[DIR]STANJAN_MAC/2005-08-14 12:39 -  
[DIR]Rocket_images/2005-02-23 19:36 -  
[DIR]References/2020-03-10 12:37 -  
[ ]Normalized Engine Thrust For Several Aircraft.pdf2017-01-31 13:02 2.1M 
[DIR]Jet_engine_images/2009-01-29 13:43 -  
[ ]JPC_HRTC_July_29_2014_Similarity_Solution.pdf2015-03-10 10:01 6.6M 
[ ]JP4_Air_CombustionFromCEA.pdf2007-02-01 00:14 50K 
[IMG]H2_O2_at100barfromCEA.jpg2007-02-26 22:38 1.0M 
[IMG]H2_O2_at50barfromCEA.jpg2007-02-26 22:31 1.0M 
[ ]Glushko, Development of Rocketry and Space Technology in the USSR.pdf2019-12-17 14:31 11M 
[ ]EnergyFromWasteNitrogen_May4_2010.pdf2010-05-21 07:30 3.7M 
[ ]Cantwell2014_Article_SimilaritySolutionOfFuelMassTransfer.pdf2020-04-06 14:07 1.1M 
[DIR]CEAforPowerPCMac/2008-03-13 08:15 -  
[DIR]CEAforIntelMac/2014-01-06 13:45 -  
[ ]A new boundary layer integral method based on the universal velocity profile PofF 2022.pdf2022-09-23 17:06 4.3M 
[ ]A_Treatise on the Motion of Rockets and an Essay on Naval Gunnery, Commentary by W Johnson.pdf2012-02-23 10:02 1.5M 
[ ]A_Treatise_on_the_Motion_of_Rockets_by_William_Moore_1813.pdf2022-07-28 16:26 5.4M 
[ ]A Single Stage to Orbit Design for a Hybrid Mars Ascent_Vehicle_2019-3840.pdf2020-07-08 13:33 941K 
[ ]A Design for a Two-Stage Solid Mars Ascent Vehicle_2019-4149.pdf2020-07-08 13:35 933K 
[ ]AA283_Turbojet_Cycle_Power_Generation_Cantwell.pdf2015-02-02 13:50 3.2M