Add to ORKGThis document consists of the presentation submitted at the Autonomous Rendezvous and Docking (ARD) Conference. The document contains three volumes: ARD hardware technology; ARD software technology; and ARD operations. The purpose of this conference is to identify the technologies required for an on orbit demonstration of ARD, assess the maturity of these technologies, and provide the necessary insight for a quality assessment of programmatic management, technical, schedule, and cost risks
This study was undertaken to determine the velocity of fragments generated by the range safety destr...
Information on the Tethered Gravity Laboratory on the International Space Station is given in viewgr...
The development of an effective satellite services system was investigated. Satek Satellite user mar...
The Timed Doppler Interferometer (TIDI) will accurately and precisely determine the global vector ML...
Autonomous Rendezvous and Docking (ARD) will be a requirement for future space programs. Clear examp...
A ground vibration test was performed on the AH-64 (Apache) helicopter to determine the frequency re...
The focus is in the development of more accurate and efficient advanced methods for solution of sing...
Under a rotorcraft structural dynamics program sponsored by the NASA Langley Research Center, Sikors...
Linear and angular vibration measurements for V/STOL aircraft, and strapdown inertial guidance syste...
The issue of technology advancement and future space transportation vehicles is addressed. The chall...
This is Volume 1, NASA Resources 1958-1968, of a multi-volume series providing a 20-year compilation...
This is the eleventh in a series of evaluated sets of rate constants and photochemical cross section...
The construction of detailed computational models of the dynamic behavior of various explosive ordna...
An annual report that summarizes the work done on Grant No. NAG2-542 is presented. There are four ar...
The utilization of the Shuttle-C Heavy Lift Launch Vehicle (HLLV) to augment the Shuttle orbiter to ...
This study was undertaken to determine the velocity of fragments generated by the range safety destr...
Information on the Tethered Gravity Laboratory on the International Space Station is given in viewgr...
The development of an effective satellite services system was investigated. Satek Satellite user mar...
The Timed Doppler Interferometer (TIDI) will accurately and precisely determine the global vector ML...
Autonomous Rendezvous and Docking (ARD) will be a requirement for future space programs. Clear examp...
A ground vibration test was performed on the AH-64 (Apache) helicopter to determine the frequency re...
The focus is in the development of more accurate and efficient advanced methods for solution of sing...
Under a rotorcraft structural dynamics program sponsored by the NASA Langley Research Center, Sikors...
Linear and angular vibration measurements for V/STOL aircraft, and strapdown inertial guidance syste...
The issue of technology advancement and future space transportation vehicles is addressed. The chall...
This is Volume 1, NASA Resources 1958-1968, of a multi-volume series providing a 20-year compilation...
This is the eleventh in a series of evaluated sets of rate constants and photochemical cross section...
The construction of detailed computational models of the dynamic behavior of various explosive ordna...
An annual report that summarizes the work done on Grant No. NAG2-542 is presented. There are four ar...
The utilization of the Shuttle-C Heavy Lift Launch Vehicle (HLLV) to augment the Shuttle orbiter to ...
This study was undertaken to determine the velocity of fragments generated by the range safety destr...
Information on the Tethered Gravity Laboratory on the International Space Station is given in viewgr...
The development of an effective satellite services system was investigated. Satek Satellite user mar...