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Box 1

 Container

Contains 92 Results:

“Iterative Guidance Applied to Generalized Missions.”, 1966

 File — Box: 1, Folder: 82
Scope and Contents From the Collection:

Documents and notes pertaining to Horn's career in missile and rocket development. Some artifacts are written in German.

Dates: 1966

“Optimization Problems Caused by Interaction of Guidance and Propellant System.”, 1963

 File — Box: 1, Folder: 83
Scope and Contents From the Collection:

Documents and notes pertaining to Horn's career in missile and rocket development. Some artifacts are written in German.

Dates: 1963

Third European Spaceflight Symposium. List of Participants. , 1964

 File — Box: 1, Folder: 84
Scope and Contents From the Collection:

Documents and notes pertaining to Horn's career in missile and rocket development. Some artifacts are written in German.

Dates: 1964

“Anwendung eines iterativen Lenkverfahren auf eine Mondlandung.” , 1965-11

 File — Box: 1, Folder: 85
Scope and Contents From the Collection:

Documents and notes pertaining to Horn's career in missile and rocket development. Some artifacts are written in German.

Dates: 1965-11

“Application of an Iterative Guidance Mode to a Lunar Landing.” NASA TN D-2967 , 1971-07-20

 File — Box: 1, Folder: 86
Scope and Contents From the Collection:

Documents and notes pertaining to Horn's career in missile and rocket development. Some artifacts are written in German.

Dates: 1971-07-20

“Mathematical Concepts and Historical Development of the Mascot Guidance Technique for Space Vehicles.” NASA TM-X64608 , 1971-07-20

 File — Box: 1, Folder: 87
Scope and Contents From the Collection:

Documents and notes pertaining to Horn's career in missile and rocket development. Some artifacts are written in German.

Dates: 1971-07-20

Space Flight Mechanics Specialist Conference. University of Denver. 1966. , 1966

 Item — Box: 1, Folder: 88
Scope and Contents • "Motion of a Vehicle in the Transition Region of the Restricted Three Body Problem (Summary)," • "Some Qualitative Characteristics of Near-Lunar Satellite Orbits," • "Orbit Determination for Stationary Satellites," • "Orbit Computation for Motion in a Non-Central Force Field," • "A Parameter Optimization Procedure for Multi-Stage Vehicles," • "A Combination Numerical-Analytical Approach to Ascent Trajectory Optimization," • "Asymptotic Matching in Power-Limited Interplanetary...
Dates: 1966

Agenda. 1) IGM Three Stage Logic Definition for S-II Terminal Stage Configuration (Dry Workshop). 2) Reformulation of Predicted Range Angle in Order to Remove Empirical Constant. 3) Thrust Filter.

 File — Box: 1, Folder: 28
Scope and Contents From the Collection:

Documents and notes pertaining to Horn's career in missile and rocket development. Some artifacts are written in German.

Dates: 1930 - 1979

Note to Mr. Horn. Continuous Guidance S-II/S-IVB , 1968-10-08

 File — Box: 1, Folder: 29
Scope and Contents From the Collection:

Documents and notes pertaining to Horn's career in missile and rocket development. Some artifacts are written in German.

Dates: 1968-10-08