AU3610300A - Single-stage-to-orbit rocket - Google Patents

Single-stage-to-orbit rocket

Info

Publication number
AU3610300A
AU3610300A AU36103/00A AU3610300A AU3610300A AU 3610300 A AU3610300 A AU 3610300A AU 36103/00 A AU36103/00 A AU 36103/00A AU 3610300 A AU3610300 A AU 3610300A AU 3610300 A AU3610300 A AU 3610300A
Authority
AU
Australia
Prior art keywords
stage
rocket
orbit
orbit rocket
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
AU36103/00A
Other languages
English (en)
Inventor
Joe A. Martin
Larry H. Welch
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Technanogy LLC
Original Assignee
Technanogy LLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Technanogy LLC filed Critical Technanogy LLC
Publication of AU3610300A publication Critical patent/AU3610300A/en
Abandoned legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/14—Space shuttles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/002—Launch systems
    • B64G1/006—Reusable launch rockets or boosters
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/403—Solid propellant rocket engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/10—Shape or structure of solid propellant charges
    • F02K9/22—Shape or structure of solid propellant charges of the front-burning type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/26—Burning control
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/28—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants having two or more propellant charges with the propulsion gases exhausting through a common nozzle

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Testing Of Engines (AREA)
AU36103/00A 1999-11-23 2000-02-29 Single-stage-to-orbit rocket Abandoned AU3610300A (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US44792699A 1999-11-23 1999-11-23
US09447926 1999-11-23
PCT/US2000/005126 WO2001038170A1 (fr) 1999-11-23 2000-02-29 Fusee monoetage volant jusqu'a l'orbite

Publications (1)

Publication Number Publication Date
AU3610300A true AU3610300A (en) 2001-06-04

Family

ID=23778298

Family Applications (1)

Application Number Title Priority Date Filing Date
AU36103/00A Abandoned AU3610300A (en) 1999-11-23 2000-02-29 Single-stage-to-orbit rocket

Country Status (2)

Country Link
AU (1) AU3610300A (fr)
WO (1) WO2001038170A1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2936570B1 (fr) * 2008-09-26 2012-10-12 Thales Sa Propulseur a combustible nano-energetique
FR3033770B1 (fr) * 2015-03-20 2018-06-15 Centre National D'etudes Spatiales (Cnes) Zone de lancement d'un engin aerospatial a propulsion a base d'un propergol solide et procede de protection associe
CN112661214B (zh) * 2020-09-30 2022-08-05 北京空间飞行器总体设计部 一种应对过载及背压的水升华器供水控制方法

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3165060A (en) * 1960-10-31 1965-01-12 James V Braun Multiple propellent grain for rocket motors
FR1510159A (fr) * 1966-12-09 1968-01-19 France Etat Nouveau bloc de propergol à combustion mixte
US3780968A (en) * 1967-01-03 1973-12-25 A Parilla Solid propellant rocket engine control and missile configurations
BE755381A (fr) * 1969-08-27 1971-02-01 Dynamit Nobel Ag Fusee pour le lancement de cables
US5172875A (en) * 1988-03-30 1992-12-22 Israel Fried Space launcher and method for launching objects into space
US5386777A (en) * 1992-02-10 1995-02-07 Aero-Jet General Corporation Rocket motor construction from porous binder core
DE4422196A1 (de) * 1994-06-24 1994-11-10 Thomas Dr Stinnesbeck Anordnung zur Nutzung von Metallhydriden in Hybridraketentriebwerken
US6612522B1 (en) * 1998-03-17 2003-09-02 Starcraft Boosters, Inc. Flyback booster with removable rocket propulsion module

Also Published As

Publication number Publication date
WO2001038170A1 (fr) 2001-05-31

Similar Documents

Publication Publication Date Title
AU1173201A (en) Skin-gripper
AU3092999A (en) Digital-timeshare-exchange
AU3385400A (en) Variable burn-rate propellant
AU5967600A (en) Candystraw
AU7514700A (en) Cyanopiperidines
AU4115400A (en) Short-circuiter
AU6335000A (en) Depthimeter
AU4497500A (en) Igniter
AU2023701A (en) Sketcher
AU2804600A (en) Arylaminoalkylamides
AU6440900A (en) Homogentisate-dioxygenase
AU2699800A (en) Organoceramics
AU6098300A (en) Follistatin-3
AU4916900A (en) Benzofuranylsulfonates
AU4561600A (en) Benzofuranylaminoalcohols
AU7904200A (en) Munition
AU1323401A (en) End-burning rocket motor
AU1901801A (en) Glucofuranoses
AU3610300A (en) Single-stage-to-orbit rocket
AU7303400A (en) Osseo-distractor
AU7513400A (en) Hydantoin-racemase
AU4435300A (en) Hula-hoop
AU2582200A (en) Windturbine
AU1915601A (en) Periotome
AU5416100A (en) Retinoscopes

Legal Events

Date Code Title Description
MK6 Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase