AUTOMATIC ANALYSIS OF LAUNCH VEHICLE FLIGHT TEST
Evaluation and checkout of saturn class launch vehicles using ibm 7090 computer
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Evaluation and checkout of saturn class launch vehicles using ibm 7090 computer
Solution to n-body space mechanics problems via numerical integration - ibm 7090 - fortran program
Ibm 7090 computer program to control prescribed changes in manned orbital spacecraft
Fortran program for computation of gas detonation parameters on IBM 7090 computer
Cloud pattern recognition system - IBM 7094 computer simulation program
IBM 7090 digital computer program for solving equations of motion for spacecraft separating from final rocket stage or another spacecraft by means of precision helical compression springs
IBM 7094 Fortran program for evaluating surface area, centroids of surface volume or masses, and moments of inertia for thin walled shells
Input and operating instructions, and sample problems for IBM 7094 computer programs - interplanetary trajectory program, n-body trajectory program, and sensitivity coefficients
Performance capability of new self-programming system, Amtran, for use with IBM 1620
IBM 7090 computer program for calculation of molecular composition formulas from mass spectrometer data
IBM-F04 Fortran program to design minimum weight fuel cell power systems for space vehicles
Fortran II IBM 7094 computer program for analytical development of planetary disturbing function
Computer program written in IBM 7090 Fortran II FOR analyzing space charge flow in electron or ion guns - operations manual
Hourly precipitation data from four weather stations over a 13-year period presented in SIPLIC form with aid of IBM 1620 computer
Flow fields about axisymmetric blunt bodies at large angles of attack calculated by IBM 7094 computer program
IBM 7044 computer program for numerical solution of flow behind nonaxisymmetric bow shock
Digital computer program for IBM 7094 computer to generate spacecraft tracking station calculations
Monte Carlo codes for IBM 7090 digital computer to calculate radiation heating in propellant tanks, and radiation environment about nuclear rocket stage