advanced ELV propulsion solutions: Cryogenic solid propellants

39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2003, Pages

  Lo, Roger E ^a   Adirim, Harry ^a   Poller, Sascha ^a   Schöyer, Herman ^a   Muss, Dieter ^b   Caramelli, Fabio ^c  

^a FHG ICT ^*

^b AIRBUS GROUP INNOVATIONS   (Germany)

^c EUROPEAN SPACE AGENCY   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

CHEMICAL PROPULSION; CRYOGENIC SOLID PROPELLANTS; DEGREE OF CONFIDENCE; EARTH-TO-ORBIT TRANSPORTATION; EUROPEAN SPACE AGENCY; HIGH-ENERGY DENSITY MATTER; LONG-TERM SOLUTIONS; SOLID ROCKET BOOSTERS;

SOLID PROPELLANTS;

PROPULSION;

EID: 84897756084     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

1. AI TR. Nr. 023/03-2003: CRYOGENIC SOLID PROPELLANT TRADE-OFF / Selection, properties, performances, ranking; Lo, Roger; Adirim, Harry; Wittig, Daniel; AI, Aerospace Institute, Berlin; ESTEC Contract 16830/02/NL/CP: "Acquisition and Evaluation of Cryo-Solid Propulsion CSP" Technical Note TN2 (39p., 23 Fig.,20Tab., 55Lit. zit.); 2 data appendices with 76 and 106 pages
2. AI TR. NO. 022/03-2003: SYSTEM STUDY: INFRASTRUCTURE, THERMAL MANAGEMENT, LAUNCH ENVIRONMENT; Harry Adirim; Roger Lo; Norbert Pilz; Armin Schildknecht, AI: Aerospace Institute, Berlin; Dieter Muss; Peter Muller-Remmers; Georg-Friedrich Reinbold, ASTRIUM GmbH, Bremen; ESA ESTEClContract No. 16830/02/NL/CP "Acquisition and Evaluation of Cryogenic Solid Propulsion", Technical Note TNI
3. "Verfahren zum Herstellen von kryogenen, monergolen Festtreibstoffen und danach erzeugte Festtreibstoffe (Procedure for Producing Cryogenic Solid Monopropellants and Solid Propellants Produced Therewith)" European patent 020901 44.3; 2002, by AI, Berlin, in validation.
4. German patents "Modulare, kryogene Feststoffraketentreibsatze mit permanentem Zundfackelgenerator (Modular Cryogenic Solid Propellant Charges with Permanent Ignition Torch)": 197 56 794.0-13 in validation and "Modulare Feststoffraketentreibsatze mit Urnmantelung, Fill-drain System, Kuhlung und Aufhangung (Modular Solid Propellant Charges with A Casing, Fill-drain System, Cooling and Suspension)", DP Nr.19822845, of 15.5.2002.
5. European patents: "Modulare Feststoffraketentreibsatze mit Urnrnantelung, Fill-drain System, Kuhlung und Aufhangung (Modular Solid-Fuel Rocket Propelling Charges With A Casing, A Fill-Drain System, Cooling and Suspension)", EU Patent EP 1080302 of 3. Juli 2002. Holder: Lo, Roger E.
6. International patents: PCT/DE99/01517 of 18.05.1999: "Modulare Feststoffraketentreibsatze mit Umrnantelung, Fill-drain-System, Kuhlung und Aufhangung (Modular Solid-Fuel Rocket Propelling Charges With A Casing, A Fill-Drain System, Cooling and Suspension)", filed for Ukraine (Patent Nr.54595 of 25.1 1.2002), Russia, Japan, India, Israel, China
7. USA: "Modular Solid-Fuel Rocket Charges with Rigid Support Casings", US Patent 6,421,999 B1 of July 23, 2002, Inventor: Roger E. Lo, filed May 18,1999
8. USA: "Modulare, kryogene Feststoffraketentreibsatze (Modular Cryogenic Solid Fuel Rocket Drive Sets)": US-Patent Nr. 6 311 479 B1 of June 21,2001
9. Rice, E.E., Final Report on Advanced System Concept for Total ISRU-based Propulsion and Power Systems for Unmanned and Manned Exploration, Orbitec Madison, Wisconsin, January 2000.
10. Lo, R., Adirim, H., Poller, S.,. Eisenreich, N., Weiser, V. and Kelzenberg, S., "Advances in Cryogenic Solid Propulsion", Paper VI 5 presented at the 31st Int. ICT conference, June 27-June 30, Karlsruhe, 2000
11. Harry Adirim, Roger Lo, Alexander Paatsch:, Next Generation High Performance, Low Pollution Launchers: Problems and Solutions", IAF-99-IAA3.3.01, Session V.3., Amsterdam, 8p, 14 Fig., 25. Ref, Okt.1999
12. Adirim, H.; Lo, R.; Knecht, T.; Reinbold, G.-F.; Poller S., Performance and Cost Evaluation of Cryogenic Solid Propulsion Systems; IAC-02-S.P.01; 53rd International Astronautical Congress, Houston, Texas, Oct. 11-19, 2002