Originally posted by cls
let's talk about motors: it seems like the ENG file format is a quasi-standard. as far as I can tell, that format was set up originally in DATA statements in Harry Stein's BASIC code. Jerry?
Stine established some but not all fields I identified.
I approached a part-time programmer named Fred Brennion with this idea in the 80's and he established the actual EDX and ALX file formats under my direction. I drove to his workplace at Excel-a-rate many times at my own expense to give him guidance on the programs I was the "publisher" of and which the co-author Charles E. Rogers agreed to "promote" with ads. We split the tiny profits. In fact, were there any profits?
So I would attribute the specific implementation to Fred Brennion.
It does an N number of relevent inflection points known as JEND points for "Jerry's endpoints". There are far more generic names for it I am sure.
Here are some of my favorite motor files.
00 MRev 01......:
01 Designation..: I40USR
02 Data date....: 07-27-90
03 Manufacturer.: U.S.ROCKETS
04 Cost.........: 60.00
05 Grain type...: CORED ENDBURNER (ME)
06 Propellant ID: 671
07 O.D..........: 2.125
08 Case Len : 8
09 Wgt Units....: G
10 Specs........: T
11 Wt Prop. gms.: 320
12 Load Wt. gms.: 512
13 Burn time....: 15.00
14 Favg Lbs.....: 9.54823
15 Favg Newtons.: 42.4705
16 TotImp Lbsecs: 143.223
17 TotImp Ntsecs: 637.058
18 REM1.........:
19 REM2.........:
20 Time /Thrust.: 0.00 44.00
20 Time /Thrust.: 3.50 5.00
20 Time /Thrust.: 14.90 5.00
20 Time /Thrust.: 15.00 0.00
61 Mass Fraction: .625
62 Isp lb/s/lb : 203.0
63 Rating.......: 637-I-42
64 Pct Full.....: 99% I
00 MRev 01......:
01 Designation..: G8USR
02 Data date....: 07-27-90
03 Manufacturer.: U.S.ROCKETS
04 Cost.........: 15.95
05 Grain type...: CORED ENDBURNER (ME)
06 Propellant ID: 671
07 O.D..........: 1.125
08 Case Len : 5
09 Wgt Units....: G
10 Specs........: T
11 Wt Prop. gms.: 60
12 Load Wt. gms.: 90
13 Burn time....: 15.01
14 Favg Lbs.....: 1.55149
15 Favg Newtons.: 6.90106
16 TotImp Lbsecs: 23.2879
17 TotImp Ntsecs: 103.585
18 REM1.........:
19 REM2.........:
20 Time /Thrust.: 0.00 6.30
20 Time /Thrust.: 1.50 1.30
20 Time /Thrust.: 15.00 1.30
20 Time /Thrust.: 15.01 0.00
61 Mass Fraction: .667
62 Isp lb/s/lb : 176.1
63 Rating.......: 104-G-7
64 Pct Full.....: 29% G
00 MRev 01......:
01 Designation..: I65USR
02 Data date....: 07-27-90
03 Manufacturer.: U.S.ROCKETS
04 Cost.........: 60.00
05 Grain type...: D
06 Propellant ID: 571
07 O.D..........: 2.125
08 Case Len : 8
09 Wgt Units....: G
10 Specs........: T
11 Wt Prop. gms.: 320
12 Load Wt. gms.: 500
13 Burn time....: 9.00
14 Favg Lbs.....: 15.1811
15 Favg Newtons.: 67.5255
16 TotImp Lbsecs: 136.63
17 TotImp Ntsecs: 607.730
18 REM1.........:
19 REM2.........:
20 Time /Thrust.: 0.00 26.00
20 Time /Thrust.: 1.50 26.00
20 Time /Thrust.: 9.00 0.00
61 Mass Fraction: .640
62 Isp lb/s/lb : 193.7
63 Rating.......: 608-I-68
64 Pct Full.....: 90% I