This work continues to develop advanced designs toward the ultimate goal of a GETAWAY SPECIAL to demonstrate economical removal of orbital debris utilizing local resources in orbit. The fundamental technical feasibility was demonstrated last year through theoretical calculations, quantitative computer animation, a solar focal point cutter, a robotic arm design and a subscale model. During this reporting period, several improvements are made in the solar cutter, such as auto track capabilities, better quality reflectors and a more versatile framework. The major advance has been in the design, fabrication and working demonstration of a ROBOTIC ARM that has several degrees of freedom. The functions were specifically tailored for the orbital debris handling. These advances are discussed here. Also a small fraction of the resources were allocated towards research in flame augmentation in SCRAMJETS for the NASP. Here, the fundamental advance was the attainment of Mach numbers up to 0.6 in the flame zone and a vastly improved injection system; the current work is expected to achieve supersonic combustion in the laboratory and an advanced monitoring system.
Autonomous space processor for orbital debris
Universities Space Research Association Summer Conference ; 1989 ; Huntsville, AL, United States
1989-01-01
Report
Keine Angabe
Englisch
Autonomous Space Processor for Orbital Debris
NTIS | 1991
|Autonomous space processor for orbital debris
NTRS | 1990
|Autonomous space processor for orbital debris
NTRS | 1990
Autonomous Space Processor for Orbital Debris
NTIS | 1990
|Autonomous space processor for orbital debris
NTRS | 1991
|