JPS4956400A - - Google Patents
Info
- Publication number
- JPS4956400A JPS4956400A JP9872672A JP9872672A JPS4956400A JP S4956400 A JPS4956400 A JP S4956400A JP 9872672 A JP9872672 A JP 9872672A JP 9872672 A JP9872672 A JP 9872672A JP S4956400 A JPS4956400 A JP S4956400A
- Authority
- JP
- Japan
- 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.)
- Pending
Links
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9872672A JPS4956400A (en:Method) | 1972-10-02 | 1972-10-02 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9872672A JPS4956400A (en:Method) | 1972-10-02 | 1972-10-02 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS4956400A true JPS4956400A (en:Method) | 1974-05-31 |
Family
ID=14227512
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP9872672A Pending JPS4956400A (en:Method) | 1972-10-02 | 1972-10-02 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS4956400A (en:Method) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5445100A (en) * | 1977-09-14 | 1979-04-10 | Nissan Motor Co Ltd | Rotary addition device of rocket |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3135479A (en) * | 1963-04-01 | 1964-06-02 | Ryan Aeronautical Co | Method of reducing velocity vector angular error of a space vehicle when thrust is applied |
-
1972
- 1972-10-02 JP JP9872672A patent/JPS4956400A/ja active Pending
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3135479A (en) * | 1963-04-01 | 1964-06-02 | Ryan Aeronautical Co | Method of reducing velocity vector angular error of a space vehicle when thrust is applied |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5445100A (en) * | 1977-09-14 | 1979-04-10 | Nissan Motor Co Ltd | Rotary addition device of rocket |