Box 1
Contains 92 Results:
No Title. Contains Definitions, Equations of Motion of Missile, Moments: Body and Wind, Forces: Body and Wind Axis, Earth Transformations, Angular Relations, Direction Cosines
Documents and notes pertaining to Horn's career in missile and rocket development. Some artifacts are written in German.
No English Title. Typed Notes and charts in German, with some terms translated to English. Translated terms are Missile Nr, Launch Pad, Receiver, Amplifier, Telemetry, Nominal Valve, Measured Valve, Nominal Time, Measured Time, Turbine Exhaust Pressure, Chamber Pressure, Propellant Pump Discharge Pressure, Pump Speed, Burnout Time, Recorder Start, End Recorder Time, Recorder End, End Fieldstrength Measure Time, Fieldstrength End, Doppler Recorder, Impact Range, Doppler Fieldstrength, Aeriel Coordinate., 1942-10-03
Documents and notes pertaining to Horn's career in missile and rocket development. Some artifacts are written in German.
Envelope of Diagrams
Documents and notes pertaining to Horn's career in missile and rocket development. Some artifacts are written in German.
Pencil notes, Labeled Working Papers 1945-1953, 1945 - 1953
Documents and notes pertaining to Horn's career in missile and rocket development. Some artifacts are written in German.
Astronautics and Aeronautics. Von Braun on Space Development. Blue Sky and Non-Blue Sky, 1972-04
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.
Note to Mr. Horn. Continuous Guidance S-II/S-IVB , 1968-10-08
Documents and notes pertaining to Horn's career in missile and rocket development. Some artifacts are written in German.
Technical Comments. Comment on "Development of the Iterative Guidance Mode with Its Application to Various Vehicles and Missions", 1967-12
Documents and notes pertaining to Horn's career in missile and rocket development. Some artifacts are written in German.
Aeroballistic Internal Note #30, 1953
Documents and notes pertaining to Horn's career in missile and rocket development. Some artifacts are written in German.