Attachment_0021__RECOMMENDATION_FOR_CHARGE_ESTABLISHMENT_&_UNIFORMITY_CALCULATIONS.pdf

PDF 138 KB Posted

Attached to
60mm, 81mm, 120mm Mortar Propelling Charges
Solicitation number
W52P1J-16-R-0134
Issued by

About this file

Attachment 0021 RECOMMENDATION FOR CHARGE ESTABLISHMENT & UNIFORMITY CALCULATIONS

View the file

Other files

File Type Posted
Attachment_0031__MINIMUM_GUARANTEED_AMOUNT_FOR_60_81_120MM_MORTAR_PROPELLING_CHARGES.pdf PDF
Attachment_0032__SCHEDULE.pdf PDF
Solicitation_W52P1J-16-R-0134_Amendment_0005.pdf PDF
RFP_W52P1J-16-R-0134_Amendment_0004.pdf PDF
RFP_W52P1J-16-R-0134_Amendment_0003.pdf PDF
RFP_W52P1J-16-R-0134_Amendment_0002.pdf PDF
RFP_W52P1J-16-R-0134_Amendment_0001.pdf PDF
Attachment_0020__52.246-4520_DRAWING_NUMBER_LISTING.PDF PDF
Attachment_0019__52.246-4520_END_ITEM_COMPONENT_LISTING.PDF PDF
Attachment_0020__52.246-4520_DRAWING_NUMBER_LISTING.PDF PDF
Attachment_0019__52.246-4520_END_ITEM_COMPONENT_LISTING.PDF PDF
Request_for_Proposal_(RFP)_W52P1J-16-R-0134_Amendment_0001.pdf PDF
Attachment_0001__PRICE_MATRIX.xlsx XLSX spreadsheet
Attachment_0011__ASC_FORM_715-7_-_HAZARDOUS_MATERIAL_FORM.pdf PDF
Attachment_0008__DD1695_-_NOTICE_OF_REVISION_(NOR).pdf PDF
Attachment_0017__SECURITY_STATEMENT_OF_WORK_-_PHYSICAL_SECURITY_STANDARDS_FOR_DOD_SECURITY_RISK_CATEGORY_III_IV_AMMUNITION_AND_EXPLOSIVES_(A&E)_AT_COCO_FACILITIES.pdf PDF
Attachment_0013__GUIDANCE_ON_DOCUMENTATION_OF_CONTRACT_DATA_REQUIREMENTS_LIST_(CDRL).pdf PDF
Attachment_0012__INSTRUCTIONS_FOR_COMPLETING_FORM_1423.pdf PDF
Attachment_0005__ADDRESS_LIST.pdf PDF
Attachment_0020__52.246-4520_DRAWING_NUMBER_LISTING.pdf PDF
Exhibit_F__CONTRACT_DATA_REQUIREMENTS_LIST_(CDRL)_-_81MM_M220_PROPELLING_CHARGE.pdf PDF
Attachment_0009__U.S._GOVERNMENT_POINT_OF_CONTACT_LISTING.pdf PDF
Attachment_0003__OPSEC_AQUISITION_PLAN.pdf PDF
Exhibit_G__CONTRACT_DATA_REQUIREMENTS_LIST_(CDRL)_-_120MM_M234A1_PROPELLING_CHARGE.pdf PDF
Exhibit_E__CONTRACT_DATA_REQUIREMENTS_LIST_(CDRL)_-_81MM_M219_PROPELLING_CHARGE.pdf PDF
Attachment_0019__52.246-4520_END_ITEM_COMPONENT_LISTING.pdf PDF
RFP_W52P1J-16-R-0134.pdf PDF
Exhibit_B__CONTRACT_DATA_REQUIREMENTS_LIST_(CDRL)_-_60MM_M235_PROPELLING_CHARGE.pdf PDF
Exhibit_D__CONTRACT_DATA_REQUIREMENTS_LIST_(CDRL)_-_81MM_M218_PROPELLING_CHARGE.pdf PDF
Attachment_0007__DD1694_-_REQUEST_FOR_VARIANCE_(RFV).pdf PDF
Attachment_0018__STATEMENT_OF_WORK_FOR_INERT_PROPELLING_CHARGES.pdf PDF
Attachment_0002__PAST_PERFORMANCE_QUESTIONNAIRE.docx DOCX document
Attachment_0010__STATISTICAL_PROCESS_CONTROL_(SPC)_TABLES.pdf PDF
Attachment_0006__DD1692_-_ENGINEERING_CHANGE_PROPOSAL_(ECP).pdf PDF
Exhibit_C__CONTRACT_DATA_REQUIREMENTS_LIST_(CDRL)_-_60MM_M236_PROPELLING_CHARGE.pdf PDF
Exhibit_A__CONTRACT_DATA_REQUIREMENTS_LIST_(CDRL)_-_60MM_M204_PROPELLING_CHARGE.pdf PDF
Show all 36

On GovTribe

Work with this file

  • Download the original file
  • Contacts named in this file
  • Similar government files
  • Ask GovTribe AI about this file

Text version

Recommendation for Charge Establishment & Uniformity Calculations

1. CHARGE ESTABLISHMENT PHASE

METHOD 1.

The linear relationship between the corrected velocity values and the charge weight is defined by the following formula:

V = mC + B where: V = target velocity m = slope of the line B = y-intercept of the line

C = charge weight

Use the following formulas to calculate the slope and intercept of the least square line:

i i i i i i i ii i i ccn vcvcn m n cmv B i i i i where: n = total number of samples ci = charge weight for ith vI = observed velocity for ith round

METHOD 2.

Use Excel XY Scatter chart (do not use a line chart): Charge weights as X-values, Velocities as the Y-values, include a trend line, include equation and R2 (trend line options).

Calculate the charge weight by solving for C:

C = (Vp - B)/m where: Vp = prescribed (target) velocity m = slope of the line B = y-intercept of the line

C = charge weight

Attachment 0021

2. UNIFORMITY PHASE CALCULATIONS

After velocity corrections are determined, Calculate the final recommended charge weight using the following formulas:

m

VV

DC UP −=

and

DCCFRC +=

It follows from these two equations that m

VV

CF UP

RC

where: C = charge weight from uniformity DC = amount of propellant adjustment required FRC = final recommended charge weight m = velocity slope from charge establishment VP = prescribed velocity VU = corrected mean velocity

FR/GE/UK/US PROPELLING CHARGES
Tolerance

It follows from these two equations that

File details come from the government source that posted it. Updated .