Big Chemical Encyclopedia

Chemical substances, components, reactions, process design ...

Articles Figures Tables About

Helicopter mode

In contrast to the vibrational effect, the rotational effect on hydrogen dissociation on Cu is much less understood, until very recently. Most 3D quantum calculations have used the plane rotor model, which is not appropriate for studying rotational effects. The studies of Refs. 113, 114, and 117 using the spherical rotor treatment have obtained important results on the effect of rotational orientation and the nuclear symmetry. The rotational orientational effect is clearly shown in Fig. 15, where reaction probabilities for different initial rotational orientation states are plotted as a function of kinetic energy. Significant enhancement of reaction probability is seen for the state with j = m ( helicopter mode) while the m = o ( cartwheel mode) is least effective for dissociation. [Pg.269]

Increased rotational energy helps to dissociate the molecule, as Figure 6.13 shows. Calculations indicate that rotational motion in a plane perpendicular to the surface (the cartwheel mode) is restricted, because it affects the interaction between the molecule and the surface. Rotation parallel to the surface (the helicopter mode ) is virtually free, however, and allows for stretching of the H-H bond as required for dissociation. [Pg.234]

The objectives of the program were to obtain reconnaissance field data therefore, the equipment was installed in traversing laboratories. For work on land, the BAMS was installed in a Volkswagen microbus or a private automobile. Airborne surveying was carried out with the equipment installed in a Jet Ranger helicopter. To traverse over water suspected to be polluted with mercury, the instrument was transferred to a boat. Each of these modes required special operating power and different methods of air intake and measurement. Careful calibration and zeroing procedures were required to obtain reliable measurements of the metallic mercury concentration in the ambient air. [Pg.84]

It includes two potential modes of transportation for off-site shipments of CWM (1) military aircraft and (2) truck. Choice of mode is based on distance to be transported and the quantity of CWM. Military aircraft is preferred, including both helicopter and fixed-wing aircraft. Helicopters are used if the distance is within the range of the helicopter without refueling or to move the CWM from the location where it is found to a military airfield for shipment by fixed-wing aircraft. [Pg.121]

Communication Communication is important in preventing friendly fire accidents. The US. Army Black Hawk helicopters carried a full array of standard avionics, radio, IFF, and radar equipment as well as communication equipment consisting of FM, UHF, and VHP radios. Each day the FM and UHF radios were keyed with classified codes to allow pilots to talk secure in encrypted mode. Tlie ACO directed that special frequendes were to be used when flying inside the TAOR. [Pg.117]

The F-15 s were equipped with avionics, communications, and electronic equipment similar to that on the Black Hawks, except that the F-15 s were equipped with HAVE QUICK II (HQ-II) frequency-hopping radios while the helicopters were not. HQ-II defeated most enemy attempts to jam transmissions by changing frequencies many times per second. Although the F-15 pilots preferred to use the more advanced HQ technology, the F-15 radios were capable of communicating in a clear, non-HQ-II mode. The ACQ directed that F-15s use the non-HQ-II frequency when specified aircraft that were not HQ-II capable flew in the TAOR. Qne factor involved in the accident was that Black Hawk helicopters (UH-60s) were not on the list of non-HQ-II aircraft that must be contacted using a non-HQ-II mode. [Pg.118]

Two F-15s were tasked that day to be the first aircraft in the TAOR and to sanitize it (check for hostile aircraft) before other coalition aircraft entered the area. The F-15s reached their final checkpoint before entering the TAOR approximately an hour after the helicopters had entered. They turned on all combat systems, switched their IFF Mode I code from 42 to 52, and switched to the TAOR radio frequency. They reported their entry into the TAOR to the AWACS. [Pg.121]

Even if they had been on the same frequency, the Air Force fighter aircraft were equipped with HAVE QUICK II (HQ-II) radios, while the Army helicopters were not. The only way the F-15 and Black Hawk pilots could have communicated would have been if the F-15 pilots switched to non-HQ mode. The procedures the pilots were given to follow did not tell them to do so. In fact, with respect to the two helicopters that were shot down, one contained an outdated version called HQ-I, which was not compatible with HQ-II. The other was equipped with HQ-II, but because not all of the Army helicopters supported HQ-II, CFAC refused to provide Army helicopter operations with the necessary cryptographic support required to synchronize their radios with the other QPC components. [Pg.124]

Snook suggests that the min comm norm contributed to the AWACS crew s general reluctance to enforce rules, contributed to AWACS not correcting Eagle Flight s improper Mode I code, and discouraged controllers from pushing helicopter pilots to the TAOR frequency when they entered Iraq because they were reluctant to say more than absolutely necessary. [Pg.152]

Determine the level of risk involved in the part. Obviously a helicopter is a more critical application than the driving link in a toy automobile but, between these extremes there is a specific hazard level associated with failure. The mode of failure and the possible danger associated with the failure must be evaluated to determine the criteria for the design performance. [Pg.284]

As mentioned above, the suppression of sticking in H2/Pd(100) by rotation is due to the cartwheel mode (mj = 0), whereas the helicopter ( w/ = J) mode enhances reactivity, i.e., quantum results suggest a strong steric effect. In order to verify this steric effect, the rotational quadrupole alignment parameter defined as ... [Pg.37]

Operational use of MTV payloads always occurs under dynamic conditions. That is, payloads do not burn in still air but are projected at velocities varying from 60 to 80 kt (hovering helicopter) to 650 kt (fast jet in afterbum mode). As boot-camp experience teaches us, a little wind will actually aid in burning combustibles, whereas excessive wind will blow out fire. In principle, the same applies to MTV flares. [Pg.186]

Seven-Eleven Japan, in order to reduce the process risks arising from variable traffic conditions in Japan, has implemented a flexible delivery strategy that utilizes trucks, motorcycles, boats, and even helicopters to ship their products from various distribution centers to their stores throughout Japan. This flexible delivery strategy has allowed Seven-Eleven Japan to ensure a Just-In-Time delivery of fresh products to its stores. This capability has helped Seven-Eleven Japan to become the most profitable convenience store in Japan. In addition, this multi-mode delivery system earned the respect of many Japanese earthquake victims in Kobe when Seven-Eleven Japan was the first company to deliver 64,000 rice balls in Kobe within 6 h by using 7 helicopters and 125 motorcycles. The reader is referred to Lee (2004) for details. [Pg.171]


See other pages where Helicopter mode is mentioned: [Pg.382]    [Pg.244]    [Pg.195]    [Pg.288]    [Pg.94]    [Pg.121]    [Pg.122]    [Pg.122]    [Pg.125]    [Pg.129]    [Pg.150]    [Pg.156]    [Pg.158]    [Pg.160]    [Pg.160]    [Pg.162]    [Pg.420]    [Pg.90]    [Pg.13]    [Pg.197]    [Pg.253]    [Pg.354]   
See also in sourсe #XX -- [ Pg.234 ]




SEARCH



Helicopter

© 2024 chempedia.info