ES261657A1 - Improvements introduced in the rockets (Machine-translation by Google Translate, not legally binding) - Google Patents
Improvements introduced in the rockets (Machine-translation by Google Translate, not legally binding)Info
- Publication number
- ES261657A1 ES261657A1 ES0261657A ES261657A ES261657A1 ES 261657 A1 ES261657 A1 ES 261657A1 ES 0261657 A ES0261657 A ES 0261657A ES 261657 A ES261657 A ES 261657A ES 261657 A1 ES261657 A1 ES 261657A1
- Authority
- ES
- Spain
- Prior art keywords
- rockets
- translation
- machine
- legally binding
- google translate
- 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.)
- Expired
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
- F42B15/01—Arrangements thereon for guidance or control
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- Gyroscopes (AREA)
- Inorganic Insulating Materials (AREA)
- Binders And Loading Units For Sheaves (AREA)
- Basic Packing Technique (AREA)
Abstract
Improvements introduced in rockets that have a gyroscopic rotor mounted on a stator, with a first propulsion load for the rocket drive and a second load for the rotor, characterized in that the second propulsion load is rotatable relative to the stator and rocket and, together with a part of the ignition means and at least one thrust nozzle, forms a component part of the rotor. (Machine-translation by Google Translate, not legally binding)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH8011159A CH375916A (en) | 1959-10-31 | 1959-10-31 | Drive for control and measuring gyroscopes, in particular for rockets |
Publications (1)
Publication Number | Publication Date |
---|---|
ES261657A1 true ES261657A1 (en) | 1960-12-16 |
Family
ID=4537661
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES0261657A Expired ES261657A1 (en) | 1959-10-31 | 1960-10-13 | Improvements introduced in the rockets (Machine-translation by Google Translate, not legally binding) |
Country Status (3)
Country | Link |
---|---|
CH (1) | CH375916A (en) |
ES (1) | ES261657A1 (en) |
NL (1) | NL257177A (en) |
-
0
- NL NL257177D patent/NL257177A/xx unknown
-
1959
- 1959-10-31 CH CH8011159A patent/CH375916A/en unknown
-
1960
- 1960-10-13 ES ES0261657A patent/ES261657A1/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
CH375916A (en) | 1964-03-15 |
NL257177A (en) |
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