Manual control of high-altitude Apollo launch abort
Simulation study of manual control capability for Apollo spacecraft reentry orientation after high altitude launch abort using visual scene
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Simulation study of manual control capability for Apollo spacecraft reentry orientation after high altitude launch abort using visual scene
Boundary curve for combinations of altitude and descent rate for safe abort during terminal phase of lunar landing
Two Project High Water experiments producing optical, ELF, RF, and radar data on ionospheric abort of large water quantities and expansion process
Static aerodynamic characteristics of aborted Apollo-Saturn V vehicle
Full-scale flight test from sea level of abort- escape system for manned Mercury capsule
Manual technique using optical device to abort manned lunar landing module in orbits compatible with concentric-flight-plan rendezvous
A 'lane change crash' is defined as a family of collisions that occurred when a driver attempts to change lane and strikes or is struck by a vehicle in the adjacent lane. One type of maneuver that is commonly used to avert a lane change crash involved aborting the intended lane change, and returning the vehicle to the original lane of the subject vehicle.
Two beam abort system candidates of the Electron-Ion Collier (EIC) Electron Storage Ring (ESR) are devised and discussed. The proposed candidates are based on an existing Lambertson magnet in RHIC inventory, or a brand-new Septum magnet. A comprehensive comparison is provided in this article in support of the Record of Decision.
Computational method for orbiting astronauts to determine required velocity for two impulse abort to landing site
Manned spacecraft control system requirements for abort problems
Translunar abort technique for nonfree-return missions
Crew survival ensurance under emergency situations during manned space flight, discussing Apollo abort system refinements
Earth centered abort program to generate optimal trajectories from specified preabort state vector to earth landing
User manual for launch abort data processing software
Effects of wind forces on thrusting launch vehicle and launch escape system for Apollo mode 1 aborts
Warning time required by Apollo spacecraft to successfully abort in event of launch vehicle explosion
Analysis of land impact problem during mode 1 aborts from Saturn 1B launch vehicle
Preliminary launch abort analysis for manned Apollo S-5 missions