Preliminary data are documented for a typical launch window opening, a typical in-plane case, and a typical launch window closing trajectory, not necessarily in the same daily launch window, for the Apollo Soyuz test project mission. The Soyuz will be launched first and the Apollo will be launched on the first opportunity, 7 hours 21 minutes later. If the Apollo is unable to be launched on the first opportunity, four additional opportunities are available at 30 hours 56 minutes, 54 hours 31 minutes, 78 hours 05 minutes, and 101 hours 40 minutes. If the Apollo cannot be launched in this time frame, no further attempt will be made to launch and rendezvous with the first Soyuz. Soyuz will then be deorbited; however, a second Soyuz was made ava...
The development of space shuttle separation devices is reviewed to illustrate the mechanisms involve...
Satellite berthing mechanism, umbilicals for fluid and electrical interfaces, EVA service platform, ...
The Gamma Guidance Algorithm which controls the inertial upper stage is described. The results of an...
The definition of standard flight segments of phases, representing flight profile components which c...
A guidance, navigation, and control system, the Simulated Shuttle Flight Test System (SS-FTS), when ...
High rate multiplexes asymmetry and jitter, data-dependent amplitude variations, and transition dens...
Stage separation dynamics of parallel staged reusable launch vehicles at Mach 3 and
More than 65 technical reports, papers, and articles published by personnel and contractors at the D...
Performance capability and vehicle dynamics of Saturn 5 launch vehicle for two engine out malfunctio...
The control parameters are defined which are to be used by the Photographic Technology Division for ...
The ascent opeational flight profile for the space transportation system 1 flight is designed (1) to...
Bladder failure analysis, diffuser tube weld examination, and failure mode reproduction tests of pro...
Requirements are presented for the ascent/descent (A/D) navigation and attitude-dependent ancillary ...
Feasibility study summary of remote manipulator for satellite repair and maintenance in orbi
The methodology and rationale used in the development of costs for engineering, manufacturing, testi...
The development of space shuttle separation devices is reviewed to illustrate the mechanisms involve...
Satellite berthing mechanism, umbilicals for fluid and electrical interfaces, EVA service platform, ...
The Gamma Guidance Algorithm which controls the inertial upper stage is described. The results of an...
The definition of standard flight segments of phases, representing flight profile components which c...
A guidance, navigation, and control system, the Simulated Shuttle Flight Test System (SS-FTS), when ...
High rate multiplexes asymmetry and jitter, data-dependent amplitude variations, and transition dens...
Stage separation dynamics of parallel staged reusable launch vehicles at Mach 3 and
More than 65 technical reports, papers, and articles published by personnel and contractors at the D...
Performance capability and vehicle dynamics of Saturn 5 launch vehicle for two engine out malfunctio...
The control parameters are defined which are to be used by the Photographic Technology Division for ...
The ascent opeational flight profile for the space transportation system 1 flight is designed (1) to...
Bladder failure analysis, diffuser tube weld examination, and failure mode reproduction tests of pro...
Requirements are presented for the ascent/descent (A/D) navigation and attitude-dependent ancillary ...
Feasibility study summary of remote manipulator for satellite repair and maintenance in orbi
The methodology and rationale used in the development of costs for engineering, manufacturing, testi...
The development of space shuttle separation devices is reviewed to illustrate the mechanisms involve...
Satellite berthing mechanism, umbilicals for fluid and electrical interfaces, EVA service platform, ...
The Gamma Guidance Algorithm which controls the inertial upper stage is described. The results of an...