Box 7
Contains 122 Results:
Solid Rocket Booster (SRB) Staging System Development, 1971 - 2014
Solid Rocket Booster Separation Information, 1978 - 2000
IA193 Solid Rocket Booster Separation Aerodynamics Hypercube Interpolator, 1978 - 2000
Per Craig, this is a key document.
Envelope with graphs, undated
Per Craig, this is a key document.
Final Hypercube Interpolator Data Printout, January 4, 1983
Per Craig, this is a key document.
STS Solid Rocket Booster Separation Aero Data Base, Hypercube Approach, July 18, 2000
Per Craig, this is a key document.
Solid Rocket Booster Separation Aero Data Base Status, Mark Craig (presentation), December 1982
Per Craig, this is a key document.
Solid Rocket Booster Separation Aero Hypercube Interpolator, presentation, Mark Craig, December 1982
Per Craig, this is a key document.
Alpha/Beta Summation Loop and Hypercube Summation Loop Data Spreadsheet , undated
Per Craig, this is a key document.
Notes, undated
Per Craig, this is a key document.
Graphs, undated
Per Craig, this is a key document.
Conversion of a Point (X*Y*) in Global Coordinates to Local Coordinates, June 12, 1982
Per Craig, this is a key document.
Generalized Equations (5-D, 32 Corners) , undated
Per Craig, this is a handwritten original.
Equations, June 22, 1982
Per Craig, this is a key document.
Table, undated
Per Craig, this is a key document.
Center Point Back-Solve From Interior Pint , undated
Handwritten original, per Craig.
Finite Element Method in Engineering Science, undated
Per Craig, this is a key document.
AIAA-82-0028, Numerical Solution of Space Shuttle Orbiter Flow Field, AIAA 20th Aerospace Sciences Meeting, Orlando, Florida, January 11 - 14, 1982
Per Craig, this is a key document.
Solid Rocket Booster Separation Test IA193 , undated
Per Craig, this is a key document.
Internal Letter, Rockwell International No. AS-GN&C/83-276, RE: IA193 SRB Separation Aerodynamic Data Base Validation, To: J. Almanza, From: H. Morgan, April 4, 1983
Per Craig, this is a key document.
Functions, Limits, Calculus Equations, undated
Per Craig, this is a key document.
Internal Letter, Rockwell International No. SAS/AERO/83-113, RE: Substantiation of New Hypercube Interpolator (EMS 290-200-434), To: W. Bornemann, From: H. Dresser, March 9, 1983
Key document, per Craig.
Several loose pages of equations (handwritten), undated
Per Craig, this is a key document.
Memo # EX32/7807-109, RE: Transmittal of Solid Rocket Booster Separation Aerodynamic Data Base, To: MSFC/SA21/Manager, Engineering Management Office, From: LA2/Manager for Systems Integration, July 21, 1978
Per Craig, this is a key document.
Solid Rocket Booster Separation Summary paper, undated
Includes original presentation and photographs.