| LDR | 01789cam a2200313Ma 4500 | ||
| 001 | 011446242 | ||
| 003 | MiAaHDL | ||
| 005 | 20141009010000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 041209s1970 dcua f000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6402610 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)646406561 |
| 040 | ⊔ | ⊔ | ‡aEGM ‡cSTF |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 086 | 0 | ⊔ | ‡aNAS 1.14:D-5825 |
| 088 | ⊔ | ⊔ | ‡aNASA-TN-D-5825 |
| 100 | 1 | ⊔ | ‡aThomas, Jerrell M. |
| 245 | 1 | 0 | ‡aMethod for calculating rocket engine structural loads / ‡cJerrell M. Thomas. |
| 246 | 3 | ⊔ | ‡aNASA TN D-5825 |
| 260 | ⊔ | ⊔ | ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration : ‡b[For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], ‡c1970. |
| 300 | ⊔ | ⊔ | ‡a9 p. : ‡bill. ; ‡c27 cm. |
| 490 | 0 | ⊔ | ‡aNASA technical note ; ‡vD-5825 |
| 520 | ⊔ | ⊔ | ‡aA method for calculating structural loads in a rocket engine-actuator-vehicle system is developed. The engine is attached to the vehicle by a universal-type gimbal joint and by two actuators. The engine is assumed to be a rigid body. Either the actuator loads or the engine angular acceleration is assumed to be known with a calculation of the other required. A set of algebraic equations is developed from which the unknown actuator loads or angular acceleration and the forces and moments at the gimbal point can be calculated . I. |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aRocket engines ‡xThrust. |
| 650 | ⊔ | 0 | ‡aRockets (Aeronautics) ‡xGuidance systems. |
| 650 | ⊔ | 0 | ‡aSpace vehicles ‡xGuidance systems. |
| 710 | 2 | ⊔ | ‡aGeorge C. Marshall Space Flight Center. |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bNational Aeronautics and Space Administration. |
| CID | ⊔ | ⊔ | ‡a011446242 |
| DAT | 0 | ⊔ | ‡a20101109162457.0 ‡b20141009010000.0 |
| DAT | 1 | ⊔ | ‡a20141112165512.0 ‡b2023-03-14T18:35:56Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
| HOL | ⊔ | ⊔ | ‡0sdr-uiuc6402610 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106881052 ‡sUIU ‡16402610 |
| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20230314 ‡sgoogle ‡uuiug.30112106881052 ‡y1970 ‡rpd ‡qbib ‡tUS fed doc |