Box 1
Contains 92 Results:
III European Space Flight Symposium Program, 1963-05
Documents and notes pertaining to Horn's career in missile and rocket development. Some artifacts are written in German.
Alabama Section 12th Annual Honors Dinner Meeting Program, 1963-11-08
Documents and notes pertaining to Horn's career in missile and rocket development. Some artifacts are written in German.
Boundary Value Problems Associated with Optimization Theory. NASA Technical Memorandum X-53365, 1965-12-03
Documents and notes pertaining to Horn's career in missile and rocket development. Some artifacts are written in German.
Optimal Ascent Into Orbit- A New Look at an Old Problem, 1964
Documents and notes pertaining to Horn's career in missile and rocket development. Some artifacts are written in German.
Cover of Astronautics The Saturn Program, 1962-02
Documents and notes pertaining to Horn's career in missile and rocket development. Some artifacts are written in German.
Handwrittten Letter to Mr. Horn Regarding The Perkins guidance report. Attached to "Flight Mechanics of Ascending Satellite Vehicles" by Frank M. Perkins, 1956-05
Documents and notes pertaining to Horn's career in missile and rocket development. Some artifacts are written in German.
Memorandum: Saturn V, Versatile in-flight targeting logic. Flow chart attached., 1966-12-16
Documents and notes pertaining to Horn's career in missile and rocket development. Some artifacts are written in German.
Pencil notes. Typed list of references., 1957 - 1963
Documents and notes pertaining to Horn's career in missile and rocket development. Some artifacts are written in German.
A New Approach to an Old Problem. First sentence is "The Influence of the gravitational field can be predicted for a vehicle in flight with a limited amount of preknowledge." Appendix A is equations. Appendix B is titled Derivation of the Average Direction of the Gravitational Vector for Elliptical Orbits
Documents and notes pertaining to Horn's career in missile and rocket development. Some artifacts are written in German.
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.
Documents and notes pertaining to Horn's career in missile and rocket development. Some artifacts are written in German.