NOTICES
Wed Jan 18 busjet.f and its input file busjet.dat are in /home/aero461/binThu Feb 23 From Shevell, page 187 I curve fit the Douglas data as e = .97 - .88(CDp)(AR) CDp = parasite drag coefficient AR = aspect ratio
Fri Feb 24 Propeller data, AIAA Handbook, Raymer, Nicolai can be checked out (not overnight) at main office, 304 Town
Fri Feb 28 Report requirements can be found from "Aircraft Project" page
Mon Mar 6 Weight subroutine errors and alterations: 1. In W2 expression: change 1.0*RKWS to 1.0+RKWS 2. In W4 expression: change 32.0+RNPA to 32.0*RNPA 3. In EPSILON expression (under 27000 ft.) change EPSILON = 1.44077*(WE**(-0.0272)) to EPSILON = .95*1.44077*(WE**(-0.0272)) NOTE: The Version in "Notes" has been corrected.
Mon Mar 27 Sign up for oral interview on your a/c design project Run /home/aero461/bin/schedule461 Note: you must see L N Wilson to change your reservation all interviews will be next week
Wed Mar 29 Info on STAR motor can be xeroxed from the copies in Rm 304. Ask the secretaries. Booster info is in AIAA Launch Vehicle Handbook in Library See anyone in Aero464 if you need other info
Mon Apr 3 When sizing the kick motor use a structural mass ratio of lambda=.2=(structure mass)/(structure mass+ propellant mass)
Mon Apr 10 The Astronomical Almanac, 1995, is in the Library Reference shelves QB8 Un3a1
Wed Apr 12 CONMAIN.f can be found in "Final Project" under "Projects"
Thur Apr 13 1. Sample CONMIN.dat 4 NDV 3 NCON 0 NSIDE 20 ITMAX 2 IPRINT .02 STEP .01 REL .01 ABS 2. See changes in "Requirements
Mon Apr 17 I have left a collection of papers on the Mars Observer Mission in 304 Town. There are papers included on the trajectory and orbit that may be of help.
Tue Apr 18 The lambda=.2 estimate applies only to the spacecraft. For the kick motor, etc., use the actual value for the STAR ( about .07)
Mon May 1 Pick up earlier projects outside Room 303, Town