Thrust modulation of ram-rockets by a vortex valve

32nd Joint Propulsion Conference and Exhibit

Volumn , Issue , 1996, Pages

  Goldman, Claudio ^a   Gany, Alon ^a  

^a TECHNION ISRAEL INSTITUTE OF TECHNOLOGY   (Israel)

Author keywords

[No Author keywords available]

Indexed keywords

GASES; HYDROGEN FUELS; MODULATION; PROPULSION; ROCKETS; SOLID PROPELLANTS; VORTEX FLOW;

CONTROLLABLE PARAMETERS; DUCTED ROCKET; FUEL-RICH SOLID PROPELLANT; MAIN PARAMETERS; MODEL PREDICTION; NOZZLE RADIUS; PROPELLANT BURNING RATE; VORTEX VALVES;

GAS GENERATORS;

EID: 85087239720     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-2624     Document Type: Conference Paper

References (10)

1. Gany, A. and Natan, B., “Optimal Fluidic Vortex Valve and Solid Propellant Combination for Variable Thrust Solid and Ducted Rockets”, Collection of Papers, 24th Israel Conf. on Aviation arid Astronautics, Feb. 17-18, 1982, pp. 238-240.
2. Natan, B., Gany, A., and Wolff, H., “Thrust Modulation of Solid Propellant Rockets by Means of a Fluidic Vortex Valve with Secondary Combustion”, Acta Astronautica, 9(12), 1982, pp. 703-711.
3. Walsh, R.F., Lewellen, W.S. and Stickler, D.B., “A Solid Propellant Rocket Motor Modulated by AFluidic Vortex Valve”, Journal of Spacecraft and Rockets, 8(1), 1971, pp. 77-79.
4. Mager, A., “Approximate Solution of Isentropic Swirling Flow Through a Nozzle”, ARS J., 31(8), 1961, pp. 1140-1148.
5. King, W.S., “On Swirling Nozzle Flows”, J of Spacecraft and Rockets, 4(10), 1967, pp. 1401-1405.
6. Lewellen, W.S., Burns, W.J., and Strickland, H.J., “Transonic Swirling Flows”, AIAA J., 7(7), 1969, pp. 1290-1297.
7. Batson, J.L. and Sforzini, R.H., “Swirling Flow Through a Nozzle”, J. of Spacecraft and Rockets, 7(2), 1970, pp. 159-163.
8. Goldman, C., and Gany, A., “Choked Swirling Flows”, TAE Report No. 773, Faculty of Aerospace Eng., Technion, Haifa, Israel, 1996.
9. Cruise, D.R., “Theoretical Computations of Equilibrium Compositions, Thermodynamic Properties, and Performance Characteristics of Propellant Systems (PEP Code)”, NWC-TP-6037, Naval Weapons Center, April 1979.
10. Chigier, N.A., and Beer, J.M., “Velocity and Static- Pressure Distribution in Swirling Air Jets Issuing from Annular and Divergent Nozzles”, J. of Basic Engineering, 86(4), 1964, pp. 788-796.