General Dynamics

About: General Dynamics is a company organization based out in Fairfax, Virginia, United States. It is known for research contribution in the topics: Signal & Propellant. The organization has 5722 authors who have published 5819 publications receiving 85768 citations. The organization is also known as: GD & General Dynamics Corporation.

Liquid-solid propulsion system and method

Abstract: A liquid-solid propulsion system having a tank of liquid oxygen and a high pressure chamber loaded with solid grain fuel with a portion of the liquid oxygen being passed through a heat exchanger to convert the liquid oxygen to gaseous oxygen. The gaseous oxygen is directed to the chamber or solid grain fuel to induce a fuel rich gas burn that is directed to a thrust chamber which also receives liquid oxygen to increase the characteristic velocity of the exhaust and thereby provide the specific impulse of the propulsion system. The gaseous oxygen is also directed to the liquid oxygen tank to pressurize the flow of liquid oxygen from the tank. Valves are interposed to control the flow of liquid and gaseous oxygen to provide the required mixture ratio in the thrust chamber for optimum specific impulse or to terminate the thrust of the propulsion system. A method for providing the liquid-solid propulsion system is also disclosed.

Method of and system for microwave interferometry

Abstract: Images of objects are obtained by microwave signal radiators and receptors which are disposed in a two dimensional array with the receptors disposed orthogonally to the radiators. The output of the receptors for illumination provided separately from each of the radiators is compared with reference microwave signals coherent with the radiated signals but varied cyclically in amplitude and phase. The results of the comparison are a plurality of outputs, which may be in digital form and which correspond to minimums in the power level of the difference signals obtained by comparison of the received signals and phase and amplitude varying reference signals. These outputs provide a two-dimensional interference pattern which can be translanted into a visual image of the object.

Thermostructural concepts for hypervelocity vehicles

Abstract: In the design of hypervelocity veh~cles (HVV). a key driving parameter is the structural mass fraction of the system. The mass fraction greatly influences the performance and payload capabilities of the vehicle. For example. a reduction of one pound of structural weight would effectively translate into an additional pound of payload, or alternatively, approximately ten fewer pounds of propellant. Through the optimization of thermostructural concepts. a significant increase in overall mission perfbrmance can be reallred. Such an optimiration requires not only good familiarity with the available material optlons and therrnostructural concepts. but also a thorough knowledge of the thermal. inertial, aerodynamic, and control loads on the vehicle as a consequence of hqpervelocity flight conditions. This optimiration process the establishment o l aeroheating and other critical loads, the consideration of material alternatives, and the formulation of thermostructural concep t wa the primary l'i~cus ol' t h ~ \ study. A suborbital vehicle (Figure I ) and the aswciated trajectory (Figure 2 ) a i described in Rckrence I were chosen as stud) baselines. These selections wcrc Idlowed b> a series of interrclated design and anal] tical tazks. during which a number of thcri~~ostructural trade \tudie\ \\el-c conducted. The primary results ol'the stud! include detailed w i g h t estlmates h r the candidate thernio~tructural concepts and the selecSUB-ORBITER SYNERGETIC PLANE CHANGE

Jet tab control mechanism for thrust vector control

Abstract: A missile jet tab actuator system for a thrust vector control coupled to aerodynamic controlled surfaces is disclosed. The device removes roll information present in commands to the aerodynamic surfaces. Only pitch and yaw information is thus supplied to the thrust vector control jet tabs. In this disclosure, the roll information is removed by a gear and slotted sleeve system. The resulting pitch and yaw output is used to drive the thrust vector control jet tabs. No separate set of independently powered actuators for such tabs is required.